Components
5
Twig Components
47
Render Count
111
ms
Render Time
82.0
MiB
Memory Usage
Components
| Name | Metadata | Render Count | Render Time |
|---|---|---|---|
| ProductCard |
"App\Twig\Components\ProductCard"components/ProductCard.html.twig |
15 | 106.64ms |
| ProductState |
"App\Twig\Components\ProductState"components/ProductState.html.twig |
15 | 3.17ms |
| ProductMostRecent |
"App\Twig\Components\ProductMostRecent"components/ProductMostRecent.html.twig |
15 | 10.80ms |
| PageBanner |
"App\Twig\Components\PageBanner"components/PageBanner.html.twig |
1 | 4.85ms |
| BackButton |
"App\Twig\Components\BackButton"components/BackButton.html.twig |
1 | 0.26ms |
Render calls
| PageBanner | App\Twig\Components\PageBanner | 82.0 MiB | 4.85 ms | |
|---|---|---|---|---|
| Input props | [ "backLabel" => "49 : Aircraft and space vehicle engineering" "backUrl" => "/taxons/main/ics-2277/49-aircraft-and-space-vehicle-engineering-4638" "paddingClasses" => "p-2 px-lg-5 py-lg-0" "searchPlaceholder" => "sylius.ui.search" "showSearch" => "true" "title" => "49.090 : On-board equipment and instruments" ] |
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| Attributes | [] |
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| Component | App\Twig\Components\PageBanner {#94335 +supTitle: null +title: "49.090 : On-board equipment and instruments" +subTitle: null +backUrl: "/taxons/main/ics-2277/49-aircraft-and-space-vehicle-engineering-4638" +backLabel: "49 : Aircraft and space vehicle engineering" +customClasses: null +backgroundType: null +centered: true +showSearch: true +searchPlaceholder: "sylius.ui.search" +searchValue: null +paddingClasses: "p-2 px-lg-5 py-lg-0" } |
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| BackButton | App\Twig\Components\BackButton | 82.0 MiB | 0.26 ms | |
|---|---|---|---|---|
| Input props | [ "url" => "/taxons/main/ics-2277/49-aircraft-and-space-vehicle-engineering-4638" "label" => "49 : Aircraft and space vehicle engineering" ] |
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| Attributes | [] |
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| Component | App\Twig\Components\BackButton {#94426 +label: "49 : Aircraft and space vehicle engineering" +url: "/taxons/main/ics-2277/49-aircraft-and-space-vehicle-engineering-4638" } |
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| ProductCard | App\Twig\Components\ProductCard | 82.0 MiB | 14.56 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#94991 #id: 8445 #code: "IEEE00000485" #attributes: Doctrine\ORM\PersistentCollection {#95052 …} #variants: Doctrine\ORM\PersistentCollection {#95050 …} #options: Doctrine\ORM\PersistentCollection {#95046 …} #associations: Doctrine\ORM\PersistentCollection {#95048 …} #createdAt: DateTime @1751037422 {#94988 : 2025-06-27 17:17:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#94994 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95062 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#95599 #locale: "en_US" #translatable: App\Entity\Product\Product {#94991} #id: 28789 #name: "IEEE 292:1969 (R2010)" #slug: "ieee-292-1969-r2010-ieee00000485-240097" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding,less than)______ (+,-,±)______ degrees per second].<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding, less than)______ (+,?,±)______ degrees per second]. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95060 …} #channels: Doctrine\ORM\PersistentCollection {#95054 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95058 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95056 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95068 …} -apiLastModifiedAt: DateTime @1754517600 {#94999 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618178400 {#95002 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @-34304400 {#95000 : 1968-11-30 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1276725600 {#94998 : 2010-06-17 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @1616626800 {#94997 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "292" -bookCollection: "" -pageCount: 16 -documents: Doctrine\ORM\PersistentCollection {#95066 …} -favorites: Doctrine\ORM\PersistentCollection {#95064 …} } "layout" => "vertical" "showPrice" => true "showStatusBadges" => true "imageFilter" => "product_listing_thumbnail" "additionalClasses" => "h-100 border-0" "hasStretchedLink" => true "backgroundColor" => "white" "hoverType" => "border-black" ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductCard {#95479 +product: App\Entity\Product\Product {#94991 #id: 8445 #code: "IEEE00000485" #attributes: Doctrine\ORM\PersistentCollection {#95052 …} #variants: Doctrine\ORM\PersistentCollection {#95050 …} #options: Doctrine\ORM\PersistentCollection {#95046 …} #associations: Doctrine\ORM\PersistentCollection {#95048 …} #createdAt: DateTime @1751037422 {#94988 : 2025-06-27 17:17:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#94994 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95062 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#95599 #locale: "en_US" #translatable: App\Entity\Product\Product {#94991} #id: 28789 #name: "IEEE 292:1969 (R2010)" #slug: "ieee-292-1969-r2010-ieee00000485-240097" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding,less than)______ (+,-,±)______ degrees per second].<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding, less than)______ (+,?,±)______ degrees per second]. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95060 …} #channels: Doctrine\ORM\PersistentCollection {#95054 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95058 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95056 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95068 …} -apiLastModifiedAt: DateTime @1754517600 {#94999 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618178400 {#95002 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @-34304400 {#95000 : 1968-11-30 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1276725600 {#94998 : 2010-06-17 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @1616626800 {#94997 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "292" -bookCollection: "" -pageCount: 16 -documents: Doctrine\ORM\PersistentCollection {#95066 …} -favorites: Doctrine\ORM\PersistentCollection {#95064 …} } +layout: "vertical" +showPrice: true +showStatusBadges: true +additionalClasses: "h-100 border-0" +linkLabel: "" +imageFilter: "product_listing_thumbnail" +hasStretchedLink: true +backgroundColor: "white" +hoverType: "border-black" } |
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| ProductState | App\Twig\Components\ProductState | 82.0 MiB | 0.36 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#94991 #id: 8445 #code: "IEEE00000485" #attributes: Doctrine\ORM\PersistentCollection {#95052 …} #variants: Doctrine\ORM\PersistentCollection {#95050 …} #options: Doctrine\ORM\PersistentCollection {#95046 …} #associations: Doctrine\ORM\PersistentCollection {#95048 …} #createdAt: DateTime @1751037422 {#94988 : 2025-06-27 17:17:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#94994 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95062 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#95599 #locale: "en_US" #translatable: App\Entity\Product\Product {#94991} #id: 28789 #name: "IEEE 292:1969 (R2010)" #slug: "ieee-292-1969-r2010-ieee00000485-240097" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding,less than)______ (+,-,±)______ degrees per second].<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding, less than)______ (+,?,±)______ degrees per second]. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95060 …} #channels: Doctrine\ORM\PersistentCollection {#95054 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95058 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95056 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95068 …} -apiLastModifiedAt: DateTime @1754517600 {#94999 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618178400 {#95002 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @-34304400 {#95000 : 1968-11-30 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1276725600 {#94998 : 2010-06-17 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @1616626800 {#94997 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "292" -bookCollection: "" -pageCount: 16 -documents: Doctrine\ORM\PersistentCollection {#95066 …} -favorites: Doctrine\ORM\PersistentCollection {#95064 …} } ] |
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| Attributes | [ "showFullLabel" => false ] |
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| Component | App\Twig\Components\ProductState {#95606 +product: App\Entity\Product\Product {#94991 #id: 8445 #code: "IEEE00000485" #attributes: Doctrine\ORM\PersistentCollection {#95052 …} #variants: Doctrine\ORM\PersistentCollection {#95050 …} #options: Doctrine\ORM\PersistentCollection {#95046 …} #associations: Doctrine\ORM\PersistentCollection {#95048 …} #createdAt: DateTime @1751037422 {#94988 : 2025-06-27 17:17:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#94994 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95062 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#95599 #locale: "en_US" #translatable: App\Entity\Product\Product {#94991} #id: 28789 #name: "IEEE 292:1969 (R2010)" #slug: "ieee-292-1969-r2010-ieee00000485-240097" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding,less than)______ (+,-,±)______ degrees per second].<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding, less than)______ (+,?,±)______ degrees per second]. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95060 …} #channels: Doctrine\ORM\PersistentCollection {#95054 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95058 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95056 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95068 …} -apiLastModifiedAt: DateTime @1754517600 {#94999 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618178400 {#95002 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @-34304400 {#95000 : 1968-11-30 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1276725600 {#94998 : 2010-06-17 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @1616626800 {#94997 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "292" -bookCollection: "" -pageCount: 16 -documents: Doctrine\ORM\PersistentCollection {#95066 …} -favorites: Doctrine\ORM\PersistentCollection {#95064 …} } +appearance: "state-withdrawn" +labels: [ "Withdrawn" ] -stateAttributeCode: "state" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductMostRecent | App\Twig\Components\ProductMostRecent | 82.0 MiB | 1.13 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#94991 #id: 8445 #code: "IEEE00000485" #attributes: Doctrine\ORM\PersistentCollection {#95052 …} #variants: Doctrine\ORM\PersistentCollection {#95050 …} #options: Doctrine\ORM\PersistentCollection {#95046 …} #associations: Doctrine\ORM\PersistentCollection {#95048 …} #createdAt: DateTime @1751037422 {#94988 : 2025-06-27 17:17:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#94994 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95062 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#95599 #locale: "en_US" #translatable: App\Entity\Product\Product {#94991} #id: 28789 #name: "IEEE 292:1969 (R2010)" #slug: "ieee-292-1969-r2010-ieee00000485-240097" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding,less than)______ (+,-,±)______ degrees per second].<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding, less than)______ (+,?,±)______ degrees per second]. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95060 …} #channels: Doctrine\ORM\PersistentCollection {#95054 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95058 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95056 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95068 …} -apiLastModifiedAt: DateTime @1754517600 {#94999 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618178400 {#95002 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @-34304400 {#95000 : 1968-11-30 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1276725600 {#94998 : 2010-06-17 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @1616626800 {#94997 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "292" -bookCollection: "" -pageCount: 16 -documents: Doctrine\ORM\PersistentCollection {#95066 …} -favorites: Doctrine\ORM\PersistentCollection {#95064 …} } ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductMostRecent {#95700 +product: App\Entity\Product\Product {#94991 #id: 8445 #code: "IEEE00000485" #attributes: Doctrine\ORM\PersistentCollection {#95052 …} #variants: Doctrine\ORM\PersistentCollection {#95050 …} #options: Doctrine\ORM\PersistentCollection {#95046 …} #associations: Doctrine\ORM\PersistentCollection {#95048 …} #createdAt: DateTime @1751037422 {#94988 : 2025-06-27 17:17:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#94994 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95062 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#95599 #locale: "en_US" #translatable: App\Entity\Product\Product {#94991} #id: 28789 #name: "IEEE 292:1969 (R2010)" #slug: "ieee-292-1969-r2010-ieee00000485-240097" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding,less than)______ (+,-,±)______ degrees per second].<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding, less than)______ (+,?,±)______ degrees per second]. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95060 …} #channels: Doctrine\ORM\PersistentCollection {#95054 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95058 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95056 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95068 …} -apiLastModifiedAt: DateTime @1754517600 {#94999 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618178400 {#95002 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @-34304400 {#95000 : 1968-11-30 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1276725600 {#94998 : 2010-06-17 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @1616626800 {#94997 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "292" -bookCollection: "" -pageCount: 16 -documents: Doctrine\ORM\PersistentCollection {#95066 …} -favorites: Doctrine\ORM\PersistentCollection {#95064 …} } +label: "Most Recent" +icon: "check-xs" -mostRecentAttributeCode: "most_recent" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductCard | App\Twig\Components\ProductCard | 82.0 MiB | 8.26 ms | |
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| Input props | [ "product" => App\Entity\Product\Product {#95013 #id: 8446 #code: "IEEE00000486" #attributes: Doctrine\ORM\PersistentCollection {#95035 …} #variants: Doctrine\ORM\PersistentCollection {#95037 …} #options: Doctrine\ORM\PersistentCollection {#95072 …} #associations: Doctrine\ORM\PersistentCollection {#95070 …} #createdAt: DateTime @1751037423 {#95044 : 2025-06-27 17:17:03.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95043 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95024 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#95930 #locale: "en_US" #translatable: App\Entity\Product\Product {#95013} #id: 28793 #name: "IEEE 293:1969 (R2010)" #slug: "ieee-293-1969-r2010-ieee00000486-240098" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n Recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered, are compiled. In some cases alternate methods for measuring a performance characteristic have been included. This standard is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Std 292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros.<br />\n \t\t\t\t<br />\n This Test Procedure is a compilation of recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered. In some cases alternate methods for measuring a performance characteristic have been included. In selecting among the alternates, attention should be paid to the intended application of the gyro, available test facilities, and the standard methods in use by the test facility. This docu\u{AD}ment is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Standards Publication No.292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros. The intent is for the specification writer to extract the applicable test conditions and equipment from Section 3 of this document for inclusion in the paragraphs concerning test conditions and equipment corresponding to paragraph 4.5 of the Specification Format. Similarly, it is intended that the writer extract the applicable test procedures from Section 4 of this Procedure for inclusion in the paragraphs concerning test procedures, corresponding to the paragraphs listed under paragraph 4.6 of the Specification Format. This Test Procedure can also be used as a guide in the prep\u{AD}aration of a rate gyro test specification, but would require reorganization into the proper Specification Format.<br />\n Blanks have been used in this document for two distinct purposes. One purpose is to provide for<br />\n selection of specific values of test parameters and their tolerances. Other blanks are to be filled<br />\n in with the number of the applicable paragraph from Requirements Section 3 of the specifi\u{AD} cation<br />\n being written.<br />\n Aerospace Industries Association EETC Report No. 5 (Revision A), "Standard Gyro Terminology"* has<br />\n been utilized in the preparation of this Test Procedure. Al\u{AD} though this Procedure is limited to<br />\n electrically energized single-degree-of-freedom spring-restrained rate gyros, it can be<br />\n used as a guide in the preparation of Test Pro\u{AD}Procedures<br />\n for other types of rate gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95027 …} #channels: Doctrine\ORM\PersistentCollection {#95033 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95029 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95031 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95010 …} -apiLastModifiedAt: DateTime @1754517600 {#95042 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618178400 {#95041 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @-34304400 {#95040 : 1968-11-30 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1276725600 {#95039 : 2010-06-17 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @1616626800 {#95015 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "293" -bookCollection: "" -pageCount: 20 -documents: Doctrine\ORM\PersistentCollection {#95008 …} -favorites: Doctrine\ORM\PersistentCollection {#95025 …} } "layout" => "vertical" "showPrice" => true "showStatusBadges" => true "imageFilter" => "product_listing_thumbnail" "additionalClasses" => "h-100 border-0" "hasStretchedLink" => true "backgroundColor" => "secondary-lighter" "hoverType" => "border-black" ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductCard {#95908 +product: App\Entity\Product\Product {#95013 #id: 8446 #code: "IEEE00000486" #attributes: Doctrine\ORM\PersistentCollection {#95035 …} #variants: Doctrine\ORM\PersistentCollection {#95037 …} #options: Doctrine\ORM\PersistentCollection {#95072 …} #associations: Doctrine\ORM\PersistentCollection {#95070 …} #createdAt: DateTime @1751037423 {#95044 : 2025-06-27 17:17:03.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95043 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95024 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#95930 #locale: "en_US" #translatable: App\Entity\Product\Product {#95013} #id: 28793 #name: "IEEE 293:1969 (R2010)" #slug: "ieee-293-1969-r2010-ieee00000486-240098" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n Recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered, are compiled. In some cases alternate methods for measuring a performance characteristic have been included. This standard is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Std 292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros.<br />\n \t\t\t\t<br />\n This Test Procedure is a compilation of recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered. In some cases alternate methods for measuring a performance characteristic have been included. In selecting among the alternates, attention should be paid to the intended application of the gyro, available test facilities, and the standard methods in use by the test facility. This docu\u{AD}ment is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Standards Publication No.292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros. The intent is for the specification writer to extract the applicable test conditions and equipment from Section 3 of this document for inclusion in the paragraphs concerning test conditions and equipment corresponding to paragraph 4.5 of the Specification Format. Similarly, it is intended that the writer extract the applicable test procedures from Section 4 of this Procedure for inclusion in the paragraphs concerning test procedures, corresponding to the paragraphs listed under paragraph 4.6 of the Specification Format. This Test Procedure can also be used as a guide in the prep\u{AD}aration of a rate gyro test specification, but would require reorganization into the proper Specification Format.<br />\n Blanks have been used in this document for two distinct purposes. One purpose is to provide for<br />\n selection of specific values of test parameters and their tolerances. Other blanks are to be filled<br />\n in with the number of the applicable paragraph from Requirements Section 3 of the specifi\u{AD} cation<br />\n being written.<br />\n Aerospace Industries Association EETC Report No. 5 (Revision A), "Standard Gyro Terminology"* has<br />\n been utilized in the preparation of this Test Procedure. Al\u{AD} though this Procedure is limited to<br />\n electrically energized single-degree-of-freedom spring-restrained rate gyros, it can be<br />\n used as a guide in the preparation of Test Pro\u{AD}Procedures<br />\n for other types of rate gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95027 …} #channels: Doctrine\ORM\PersistentCollection {#95033 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95029 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95031 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95010 …} -apiLastModifiedAt: DateTime @1754517600 {#95042 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618178400 {#95041 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @-34304400 {#95040 : 1968-11-30 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1276725600 {#95039 : 2010-06-17 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @1616626800 {#95015 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "293" -bookCollection: "" -pageCount: 20 -documents: Doctrine\ORM\PersistentCollection {#95008 …} -favorites: Doctrine\ORM\PersistentCollection {#95025 …} } +layout: "vertical" +showPrice: true +showStatusBadges: true +additionalClasses: "h-100 border-0" +linkLabel: "" +imageFilter: "product_listing_thumbnail" +hasStretchedLink: true +backgroundColor: "secondary-lighter" +hoverType: "border-black" } |
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| ProductState | App\Twig\Components\ProductState | 82.0 MiB | 0.27 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95013 #id: 8446 #code: "IEEE00000486" #attributes: Doctrine\ORM\PersistentCollection {#95035 …} #variants: Doctrine\ORM\PersistentCollection {#95037 …} #options: Doctrine\ORM\PersistentCollection {#95072 …} #associations: Doctrine\ORM\PersistentCollection {#95070 …} #createdAt: DateTime @1751037423 {#95044 : 2025-06-27 17:17:03.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95043 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95024 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#95930 #locale: "en_US" #translatable: App\Entity\Product\Product {#95013} #id: 28793 #name: "IEEE 293:1969 (R2010)" #slug: "ieee-293-1969-r2010-ieee00000486-240098" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n Recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered, are compiled. In some cases alternate methods for measuring a performance characteristic have been included. This standard is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Std 292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros.<br />\n \t\t\t\t<br />\n This Test Procedure is a compilation of recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered. In some cases alternate methods for measuring a performance characteristic have been included. In selecting among the alternates, attention should be paid to the intended application of the gyro, available test facilities, and the standard methods in use by the test facility. This docu\u{AD}ment is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Standards Publication No.292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros. The intent is for the specification writer to extract the applicable test conditions and equipment from Section 3 of this document for inclusion in the paragraphs concerning test conditions and equipment corresponding to paragraph 4.5 of the Specification Format. Similarly, it is intended that the writer extract the applicable test procedures from Section 4 of this Procedure for inclusion in the paragraphs concerning test procedures, corresponding to the paragraphs listed under paragraph 4.6 of the Specification Format. This Test Procedure can also be used as a guide in the prep\u{AD}aration of a rate gyro test specification, but would require reorganization into the proper Specification Format.<br />\n Blanks have been used in this document for two distinct purposes. One purpose is to provide for<br />\n selection of specific values of test parameters and their tolerances. Other blanks are to be filled<br />\n in with the number of the applicable paragraph from Requirements Section 3 of the specifi\u{AD} cation<br />\n being written.<br />\n Aerospace Industries Association EETC Report No. 5 (Revision A), "Standard Gyro Terminology"* has<br />\n been utilized in the preparation of this Test Procedure. Al\u{AD} though this Procedure is limited to<br />\n electrically energized single-degree-of-freedom spring-restrained rate gyros, it can be<br />\n used as a guide in the preparation of Test Pro\u{AD}Procedures<br />\n for other types of rate gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95027 …} #channels: Doctrine\ORM\PersistentCollection {#95033 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95029 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95031 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95010 …} -apiLastModifiedAt: DateTime @1754517600 {#95042 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618178400 {#95041 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @-34304400 {#95040 : 1968-11-30 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1276725600 {#95039 : 2010-06-17 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @1616626800 {#95015 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "293" -bookCollection: "" -pageCount: 20 -documents: Doctrine\ORM\PersistentCollection {#95008 …} -favorites: Doctrine\ORM\PersistentCollection {#95025 …} } ] |
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| Attributes | [ "showFullLabel" => false ] |
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| Component | App\Twig\Components\ProductState {#95944 +product: App\Entity\Product\Product {#95013 #id: 8446 #code: "IEEE00000486" #attributes: Doctrine\ORM\PersistentCollection {#95035 …} #variants: Doctrine\ORM\PersistentCollection {#95037 …} #options: Doctrine\ORM\PersistentCollection {#95072 …} #associations: Doctrine\ORM\PersistentCollection {#95070 …} #createdAt: DateTime @1751037423 {#95044 : 2025-06-27 17:17:03.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95043 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95024 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#95930 #locale: "en_US" #translatable: App\Entity\Product\Product {#95013} #id: 28793 #name: "IEEE 293:1969 (R2010)" #slug: "ieee-293-1969-r2010-ieee00000486-240098" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n Recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered, are compiled. In some cases alternate methods for measuring a performance characteristic have been included. This standard is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Std 292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros.<br />\n \t\t\t\t<br />\n This Test Procedure is a compilation of recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered. In some cases alternate methods for measuring a performance characteristic have been included. In selecting among the alternates, attention should be paid to the intended application of the gyro, available test facilities, and the standard methods in use by the test facility. This docu\u{AD}ment is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Standards Publication No.292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros. The intent is for the specification writer to extract the applicable test conditions and equipment from Section 3 of this document for inclusion in the paragraphs concerning test conditions and equipment corresponding to paragraph 4.5 of the Specification Format. Similarly, it is intended that the writer extract the applicable test procedures from Section 4 of this Procedure for inclusion in the paragraphs concerning test procedures, corresponding to the paragraphs listed under paragraph 4.6 of the Specification Format. This Test Procedure can also be used as a guide in the prep\u{AD}aration of a rate gyro test specification, but would require reorganization into the proper Specification Format.<br />\n Blanks have been used in this document for two distinct purposes. One purpose is to provide for<br />\n selection of specific values of test parameters and their tolerances. Other blanks are to be filled<br />\n in with the number of the applicable paragraph from Requirements Section 3 of the specifi\u{AD} cation<br />\n being written.<br />\n Aerospace Industries Association EETC Report No. 5 (Revision A), "Standard Gyro Terminology"* has<br />\n been utilized in the preparation of this Test Procedure. Al\u{AD} though this Procedure is limited to<br />\n electrically energized single-degree-of-freedom spring-restrained rate gyros, it can be<br />\n used as a guide in the preparation of Test Pro\u{AD}Procedures<br />\n for other types of rate gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95027 …} #channels: Doctrine\ORM\PersistentCollection {#95033 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95029 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95031 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95010 …} -apiLastModifiedAt: DateTime @1754517600 {#95042 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618178400 {#95041 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @-34304400 {#95040 : 1968-11-30 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1276725600 {#95039 : 2010-06-17 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @1616626800 {#95015 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "293" -bookCollection: "" -pageCount: 20 -documents: Doctrine\ORM\PersistentCollection {#95008 …} -favorites: Doctrine\ORM\PersistentCollection {#95025 …} } +appearance: "state-withdrawn" +labels: [ "Withdrawn" ] -stateAttributeCode: "state" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductMostRecent | App\Twig\Components\ProductMostRecent | 82.0 MiB | 0.93 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95013 #id: 8446 #code: "IEEE00000486" #attributes: Doctrine\ORM\PersistentCollection {#95035 …} #variants: Doctrine\ORM\PersistentCollection {#95037 …} #options: Doctrine\ORM\PersistentCollection {#95072 …} #associations: Doctrine\ORM\PersistentCollection {#95070 …} #createdAt: DateTime @1751037423 {#95044 : 2025-06-27 17:17:03.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95043 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95024 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#95930 #locale: "en_US" #translatable: App\Entity\Product\Product {#95013} #id: 28793 #name: "IEEE 293:1969 (R2010)" #slug: "ieee-293-1969-r2010-ieee00000486-240098" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n Recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered, are compiled. In some cases alternate methods for measuring a performance characteristic have been included. This standard is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Std 292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros.<br />\n \t\t\t\t<br />\n This Test Procedure is a compilation of recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered. In some cases alternate methods for measuring a performance characteristic have been included. In selecting among the alternates, attention should be paid to the intended application of the gyro, available test facilities, and the standard methods in use by the test facility. This docu\u{AD}ment is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Standards Publication No.292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros. The intent is for the specification writer to extract the applicable test conditions and equipment from Section 3 of this document for inclusion in the paragraphs concerning test conditions and equipment corresponding to paragraph 4.5 of the Specification Format. Similarly, it is intended that the writer extract the applicable test procedures from Section 4 of this Procedure for inclusion in the paragraphs concerning test procedures, corresponding to the paragraphs listed under paragraph 4.6 of the Specification Format. This Test Procedure can also be used as a guide in the prep\u{AD}aration of a rate gyro test specification, but would require reorganization into the proper Specification Format.<br />\n Blanks have been used in this document for two distinct purposes. One purpose is to provide for<br />\n selection of specific values of test parameters and their tolerances. Other blanks are to be filled<br />\n in with the number of the applicable paragraph from Requirements Section 3 of the specifi\u{AD} cation<br />\n being written.<br />\n Aerospace Industries Association EETC Report No. 5 (Revision A), "Standard Gyro Terminology"* has<br />\n been utilized in the preparation of this Test Procedure. Al\u{AD} though this Procedure is limited to<br />\n electrically energized single-degree-of-freedom spring-restrained rate gyros, it can be<br />\n used as a guide in the preparation of Test Pro\u{AD}Procedures<br />\n for other types of rate gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95027 …} #channels: Doctrine\ORM\PersistentCollection {#95033 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95029 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95031 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95010 …} -apiLastModifiedAt: DateTime @1754517600 {#95042 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618178400 {#95041 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @-34304400 {#95040 : 1968-11-30 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1276725600 {#95039 : 2010-06-17 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @1616626800 {#95015 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "293" -bookCollection: "" -pageCount: 20 -documents: Doctrine\ORM\PersistentCollection {#95008 …} -favorites: Doctrine\ORM\PersistentCollection {#95025 …} } ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductMostRecent {#96018 +product: App\Entity\Product\Product {#95013 #id: 8446 #code: "IEEE00000486" #attributes: Doctrine\ORM\PersistentCollection {#95035 …} #variants: Doctrine\ORM\PersistentCollection {#95037 …} #options: Doctrine\ORM\PersistentCollection {#95072 …} #associations: Doctrine\ORM\PersistentCollection {#95070 …} #createdAt: DateTime @1751037423 {#95044 : 2025-06-27 17:17:03.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95043 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95024 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#95930 #locale: "en_US" #translatable: App\Entity\Product\Product {#95013} #id: 28793 #name: "IEEE 293:1969 (R2010)" #slug: "ieee-293-1969-r2010-ieee00000486-240098" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n Recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered, are compiled. In some cases alternate methods for measuring a performance characteristic have been included. This standard is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Std 292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros.<br />\n \t\t\t\t<br />\n This Test Procedure is a compilation of recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered. In some cases alternate methods for measuring a performance characteristic have been included. In selecting among the alternates, attention should be paid to the intended application of the gyro, available test facilities, and the standard methods in use by the test facility. This docu\u{AD}ment is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Standards Publication No.292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros. The intent is for the specification writer to extract the applicable test conditions and equipment from Section 3 of this document for inclusion in the paragraphs concerning test conditions and equipment corresponding to paragraph 4.5 of the Specification Format. Similarly, it is intended that the writer extract the applicable test procedures from Section 4 of this Procedure for inclusion in the paragraphs concerning test procedures, corresponding to the paragraphs listed under paragraph 4.6 of the Specification Format. This Test Procedure can also be used as a guide in the prep\u{AD}aration of a rate gyro test specification, but would require reorganization into the proper Specification Format.<br />\n Blanks have been used in this document for two distinct purposes. One purpose is to provide for<br />\n selection of specific values of test parameters and their tolerances. Other blanks are to be filled<br />\n in with the number of the applicable paragraph from Requirements Section 3 of the specifi\u{AD} cation<br />\n being written.<br />\n Aerospace Industries Association EETC Report No. 5 (Revision A), "Standard Gyro Terminology"* has<br />\n been utilized in the preparation of this Test Procedure. Al\u{AD} though this Procedure is limited to<br />\n electrically energized single-degree-of-freedom spring-restrained rate gyros, it can be<br />\n used as a guide in the preparation of Test Pro\u{AD}Procedures<br />\n for other types of rate gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95027 …} #channels: Doctrine\ORM\PersistentCollection {#95033 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95029 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95031 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95010 …} -apiLastModifiedAt: DateTime @1754517600 {#95042 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618178400 {#95041 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @-34304400 {#95040 : 1968-11-30 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1276725600 {#95039 : 2010-06-17 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @1616626800 {#95015 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "293" -bookCollection: "" -pageCount: 20 -documents: Doctrine\ORM\PersistentCollection {#95008 …} -favorites: Doctrine\ORM\PersistentCollection {#95025 …} } +label: "Most Recent" +icon: "check-xs" -mostRecentAttributeCode: "most_recent" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductCard | App\Twig\Components\ProductCard | 82.0 MiB | 8.13 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95080 #id: 8623 #code: "IEEE00000760" #attributes: Doctrine\ORM\PersistentCollection {#95097 …} #variants: Doctrine\ORM\PersistentCollection {#95099 …} #options: Doctrine\ORM\PersistentCollection {#95103 …} #associations: Doctrine\ORM\PersistentCollection {#95101 …} #createdAt: DateTime @1751037571 {#95074 : 2025-06-27 17:19:31.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95075 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95087 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#96160 #locale: "en_US" #translatable: App\Entity\Product\Product {#95080} #id: 29501 #name: "IEEE 517:1974 (R2010)" #slug: "ieee-517-1974-r2010-ieee00000760-240275" #description: """ New IEEE Standard - Active.<br />\n A specification format guide for the preparation of a rate-integrating gyro specification that provides a common meeting ground of terminology and practice for manufacturers and users is presented. A compilation of recommended procedures for testing a rate-integrating gyro is given. An errata is available at http://standards.ieee.org/reading/ieee/updates/errata/517-1974_errata.pdf<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a sensor in [an attitude control system, a gimbal platform, an angular displacement measuring system, an angular rate measuring system, _________________________.] The external electronics or control system are not considered to be part of the gyro.<br />\n This standard is consists of two parts. Part I is a specification format guide for the preparation of a rate-integrating gyro specification. It provides a common meeting ground of terminology and practice for manufacturers and users. The user is cautioned not to over specify; only those parameters that are required to guarantee proper instrument performance in the specific application should be controlled. In general, the specification should contain only those requirements that can be verified by test or inspection. Parameters in addition to those given in this standard are not precluded. Figs 1 and 2 are to be used as a guide for the preparation of specific figures or drawings.<br />\n Part II is a compilation of recommended procedures for testing a rate-integrating gyro. These procedures, including test conditions to be considered, are derived from those currently in use. For a specific application, the test procedure should reflect the requirements of the specifications; thereefore, not all tests outlined in this document need be included, nor are additional tests precluded. In some cases, alternative methods for measuring performance characteristics have been included or indicated. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95089 …} #channels: Doctrine\ORM\PersistentCollection {#95095 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95091 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95093 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95081 …} -apiLastModifiedAt: DateTime @1754517600 {#95076 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95077 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @151196400 {#95078 : 1974-10-17 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1285797600 {#95079 : 2010-09-30 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: null -edition: null -coreDocument: "517" -bookCollection: "" -pageCount: 60 -documents: Doctrine\ORM\PersistentCollection {#95083 …} -favorites: Doctrine\ORM\PersistentCollection {#95085 …} } "layout" => "vertical" "showPrice" => true "showStatusBadges" => true "imageFilter" => "product_listing_thumbnail" "additionalClasses" => "h-100 border-0" "hasStretchedLink" => true "backgroundColor" => "white" "hoverType" => "border-black" ] |
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| Component | App\Twig\Components\ProductCard {#96140 +product: App\Entity\Product\Product {#95080 #id: 8623 #code: "IEEE00000760" #attributes: Doctrine\ORM\PersistentCollection {#95097 …} #variants: Doctrine\ORM\PersistentCollection {#95099 …} #options: Doctrine\ORM\PersistentCollection {#95103 …} #associations: Doctrine\ORM\PersistentCollection {#95101 …} #createdAt: DateTime @1751037571 {#95074 : 2025-06-27 17:19:31.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95075 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95087 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#96160 #locale: "en_US" #translatable: App\Entity\Product\Product {#95080} #id: 29501 #name: "IEEE 517:1974 (R2010)" #slug: "ieee-517-1974-r2010-ieee00000760-240275" #description: """ New IEEE Standard - Active.<br />\n A specification format guide for the preparation of a rate-integrating gyro specification that provides a common meeting ground of terminology and practice for manufacturers and users is presented. A compilation of recommended procedures for testing a rate-integrating gyro is given. An errata is available at http://standards.ieee.org/reading/ieee/updates/errata/517-1974_errata.pdf<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a sensor in [an attitude control system, a gimbal platform, an angular displacement measuring system, an angular rate measuring system, _________________________.] The external electronics or control system are not considered to be part of the gyro.<br />\n This standard is consists of two parts. Part I is a specification format guide for the preparation of a rate-integrating gyro specification. It provides a common meeting ground of terminology and practice for manufacturers and users. The user is cautioned not to over specify; only those parameters that are required to guarantee proper instrument performance in the specific application should be controlled. In general, the specification should contain only those requirements that can be verified by test or inspection. Parameters in addition to those given in this standard are not precluded. Figs 1 and 2 are to be used as a guide for the preparation of specific figures or drawings.<br />\n Part II is a compilation of recommended procedures for testing a rate-integrating gyro. These procedures, including test conditions to be considered, are derived from those currently in use. For a specific application, the test procedure should reflect the requirements of the specifications; thereefore, not all tests outlined in this document need be included, nor are additional tests precluded. In some cases, alternative methods for measuring performance characteristics have been included or indicated. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95089 …} #channels: Doctrine\ORM\PersistentCollection {#95095 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95091 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95093 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95081 …} -apiLastModifiedAt: DateTime @1754517600 {#95076 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95077 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @151196400 {#95078 : 1974-10-17 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1285797600 {#95079 : 2010-09-30 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: null -edition: null -coreDocument: "517" -bookCollection: "" -pageCount: 60 -documents: Doctrine\ORM\PersistentCollection {#95083 …} -favorites: Doctrine\ORM\PersistentCollection {#95085 …} } +layout: "vertical" +showPrice: true +showStatusBadges: true +additionalClasses: "h-100 border-0" +linkLabel: "" +imageFilter: "product_listing_thumbnail" +hasStretchedLink: true +backgroundColor: "white" +hoverType: "border-black" } |
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| ProductState | App\Twig\Components\ProductState | 82.0 MiB | 0.25 ms | |
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| Input props | [ "product" => App\Entity\Product\Product {#95080 #id: 8623 #code: "IEEE00000760" #attributes: Doctrine\ORM\PersistentCollection {#95097 …} #variants: Doctrine\ORM\PersistentCollection {#95099 …} #options: Doctrine\ORM\PersistentCollection {#95103 …} #associations: Doctrine\ORM\PersistentCollection {#95101 …} #createdAt: DateTime @1751037571 {#95074 : 2025-06-27 17:19:31.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95075 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95087 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#96160 #locale: "en_US" #translatable: App\Entity\Product\Product {#95080} #id: 29501 #name: "IEEE 517:1974 (R2010)" #slug: "ieee-517-1974-r2010-ieee00000760-240275" #description: """ New IEEE Standard - Active.<br />\n A specification format guide for the preparation of a rate-integrating gyro specification that provides a common meeting ground of terminology and practice for manufacturers and users is presented. A compilation of recommended procedures for testing a rate-integrating gyro is given. An errata is available at http://standards.ieee.org/reading/ieee/updates/errata/517-1974_errata.pdf<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a sensor in [an attitude control system, a gimbal platform, an angular displacement measuring system, an angular rate measuring system, _________________________.] The external electronics or control system are not considered to be part of the gyro.<br />\n This standard is consists of two parts. Part I is a specification format guide for the preparation of a rate-integrating gyro specification. It provides a common meeting ground of terminology and practice for manufacturers and users. The user is cautioned not to over specify; only those parameters that are required to guarantee proper instrument performance in the specific application should be controlled. In general, the specification should contain only those requirements that can be verified by test or inspection. Parameters in addition to those given in this standard are not precluded. Figs 1 and 2 are to be used as a guide for the preparation of specific figures or drawings.<br />\n Part II is a compilation of recommended procedures for testing a rate-integrating gyro. These procedures, including test conditions to be considered, are derived from those currently in use. For a specific application, the test procedure should reflect the requirements of the specifications; thereefore, not all tests outlined in this document need be included, nor are additional tests precluded. In some cases, alternative methods for measuring performance characteristics have been included or indicated. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95089 …} #channels: Doctrine\ORM\PersistentCollection {#95095 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95091 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95093 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95081 …} -apiLastModifiedAt: DateTime @1754517600 {#95076 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95077 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @151196400 {#95078 : 1974-10-17 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1285797600 {#95079 : 2010-09-30 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: null -edition: null -coreDocument: "517" -bookCollection: "" -pageCount: 60 -documents: Doctrine\ORM\PersistentCollection {#95083 …} -favorites: Doctrine\ORM\PersistentCollection {#95085 …} } ] |
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| Attributes | [ "showFullLabel" => false ] |
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| ProductMostRecent | App\Twig\Components\ProductMostRecent | 82.0 MiB | 0.94 ms | |
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| Input props | [ "product" => App\Entity\Product\Product {#95080 #id: 8623 #code: "IEEE00000760" #attributes: Doctrine\ORM\PersistentCollection {#95097 …} #variants: Doctrine\ORM\PersistentCollection {#95099 …} #options: Doctrine\ORM\PersistentCollection {#95103 …} #associations: Doctrine\ORM\PersistentCollection {#95101 …} #createdAt: DateTime @1751037571 {#95074 : 2025-06-27 17:19:31.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95075 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95087 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#96160 #locale: "en_US" #translatable: App\Entity\Product\Product {#95080} #id: 29501 #name: "IEEE 517:1974 (R2010)" #slug: "ieee-517-1974-r2010-ieee00000760-240275" #description: """ New IEEE Standard - Active.<br />\n A specification format guide for the preparation of a rate-integrating gyro specification that provides a common meeting ground of terminology and practice for manufacturers and users is presented. A compilation of recommended procedures for testing a rate-integrating gyro is given. An errata is available at http://standards.ieee.org/reading/ieee/updates/errata/517-1974_errata.pdf<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a sensor in [an attitude control system, a gimbal platform, an angular displacement measuring system, an angular rate measuring system, _________________________.] The external electronics or control system are not considered to be part of the gyro.<br />\n This standard is consists of two parts. Part I is a specification format guide for the preparation of a rate-integrating gyro specification. It provides a common meeting ground of terminology and practice for manufacturers and users. The user is cautioned not to over specify; only those parameters that are required to guarantee proper instrument performance in the specific application should be controlled. In general, the specification should contain only those requirements that can be verified by test or inspection. Parameters in addition to those given in this standard are not precluded. Figs 1 and 2 are to be used as a guide for the preparation of specific figures or drawings.<br />\n Part II is a compilation of recommended procedures for testing a rate-integrating gyro. These procedures, including test conditions to be considered, are derived from those currently in use. For a specific application, the test procedure should reflect the requirements of the specifications; thereefore, not all tests outlined in this document need be included, nor are additional tests precluded. In some cases, alternative methods for measuring performance characteristics have been included or indicated. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95089 …} #channels: Doctrine\ORM\PersistentCollection {#95095 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95091 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95093 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95081 …} -apiLastModifiedAt: DateTime @1754517600 {#95076 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95077 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @151196400 {#95078 : 1974-10-17 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1285797600 {#95079 : 2010-09-30 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: null -edition: null -coreDocument: "517" -bookCollection: "" -pageCount: 60 -documents: Doctrine\ORM\PersistentCollection {#95083 …} -favorites: Doctrine\ORM\PersistentCollection {#95085 …} } ] |
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| ProductCard | App\Twig\Components\ProductCard | 82.0 MiB | 8.27 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95112 #id: 8638 #code: "IEEE00000781" #attributes: Doctrine\ORM\PersistentCollection {#95129 …} #variants: Doctrine\ORM\PersistentCollection {#95131 …} #options: Doctrine\ORM\PersistentCollection {#95135 …} #associations: Doctrine\ORM\PersistentCollection {#95133 …} #createdAt: DateTime @1751037584 {#95105 : 2025-06-27 17:19:44.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95106 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95119 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#96390 #locale: "en_US" #translatable: App\Entity\Product\Product {#95112} #id: 29561 #name: "IEEE 529:1980 (R2010)" #slug: "ieee-529-1980-r2010-ieee00000781-240290" #description: """ New IEEE Standard - Active.<br />\n A specification format guide for the preparation of a rate-integrating gyroscope specification is presented. Recommended procedures for testing a rate-integrating gyroscope are compiled. This standard, when combined with IEEE Std 517-1974 (R1980), defines the requirements and test procedures in terms of characteristics unique to the gyroscope or those applications in which the dynamic angular inputs are significantly greater than the limitations identified in IEEE Std 517. (An errata is available for this standard at http://standards.ieee.org/findstds/errata/529-1980.pdf)<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a strapdown sensor for an [inertial navigation system, an attitude reference unit,__________] in an [aircraft, missile,__________] application. The characteristics of the external capture electronics are considered where necessary to define gyro performance. """ #metaKeywords: null #metaDescription: null #shortDescription: "Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95121 …} #channels: Doctrine\ORM\PersistentCollection {#95127 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95123 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95125 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95113 …} -apiLastModifiedAt: DateTime @1754517600 {#95107 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95108 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @349570800 {#95109 : 1981-01-29 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1285797600 {#95110 : 2010-09-30 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @349570800 {#95111 : 1981-01-29 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "529" -bookCollection: "" -pageCount: 24 -documents: Doctrine\ORM\PersistentCollection {#95115 …} -favorites: Doctrine\ORM\PersistentCollection {#95117 …} } "layout" => "vertical" "showPrice" => true "showStatusBadges" => true "imageFilter" => "product_listing_thumbnail" "additionalClasses" => "h-100 border-0" "hasStretchedLink" => true "backgroundColor" => "secondary-lighter" "hoverType" => "border-black" ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductCard {#96370 +product: App\Entity\Product\Product {#95112 #id: 8638 #code: "IEEE00000781" #attributes: Doctrine\ORM\PersistentCollection {#95129 …} #variants: Doctrine\ORM\PersistentCollection {#95131 …} #options: Doctrine\ORM\PersistentCollection {#95135 …} #associations: Doctrine\ORM\PersistentCollection {#95133 …} #createdAt: DateTime @1751037584 {#95105 : 2025-06-27 17:19:44.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95106 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95119 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#96390 #locale: "en_US" #translatable: App\Entity\Product\Product {#95112} #id: 29561 #name: "IEEE 529:1980 (R2010)" #slug: "ieee-529-1980-r2010-ieee00000781-240290" #description: """ New IEEE Standard - Active.<br />\n A specification format guide for the preparation of a rate-integrating gyroscope specification is presented. Recommended procedures for testing a rate-integrating gyroscope are compiled. This standard, when combined with IEEE Std 517-1974 (R1980), defines the requirements and test procedures in terms of characteristics unique to the gyroscope or those applications in which the dynamic angular inputs are significantly greater than the limitations identified in IEEE Std 517. (An errata is available for this standard at http://standards.ieee.org/findstds/errata/529-1980.pdf)<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a strapdown sensor for an [inertial navigation system, an attitude reference unit,__________] in an [aircraft, missile,__________] application. The characteristics of the external capture electronics are considered where necessary to define gyro performance. """ #metaKeywords: null #metaDescription: null #shortDescription: "Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95121 …} #channels: Doctrine\ORM\PersistentCollection {#95127 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95123 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95125 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95113 …} -apiLastModifiedAt: DateTime @1754517600 {#95107 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95108 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @349570800 {#95109 : 1981-01-29 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1285797600 {#95110 : 2010-09-30 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @349570800 {#95111 : 1981-01-29 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "529" -bookCollection: "" -pageCount: 24 -documents: Doctrine\ORM\PersistentCollection {#95115 …} -favorites: Doctrine\ORM\PersistentCollection {#95117 …} } +layout: "vertical" +showPrice: true +showStatusBadges: true +additionalClasses: "h-100 border-0" +linkLabel: "" +imageFilter: "product_listing_thumbnail" +hasStretchedLink: true +backgroundColor: "secondary-lighter" +hoverType: "border-black" } |
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| ProductState | App\Twig\Components\ProductState | 82.0 MiB | 0.26 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95112 #id: 8638 #code: "IEEE00000781" #attributes: Doctrine\ORM\PersistentCollection {#95129 …} #variants: Doctrine\ORM\PersistentCollection {#95131 …} #options: Doctrine\ORM\PersistentCollection {#95135 …} #associations: Doctrine\ORM\PersistentCollection {#95133 …} #createdAt: DateTime @1751037584 {#95105 : 2025-06-27 17:19:44.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95106 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95119 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#96390 #locale: "en_US" #translatable: App\Entity\Product\Product {#95112} #id: 29561 #name: "IEEE 529:1980 (R2010)" #slug: "ieee-529-1980-r2010-ieee00000781-240290" #description: """ New IEEE Standard - Active.<br />\n A specification format guide for the preparation of a rate-integrating gyroscope specification is presented. Recommended procedures for testing a rate-integrating gyroscope are compiled. This standard, when combined with IEEE Std 517-1974 (R1980), defines the requirements and test procedures in terms of characteristics unique to the gyroscope or those applications in which the dynamic angular inputs are significantly greater than the limitations identified in IEEE Std 517. (An errata is available for this standard at http://standards.ieee.org/findstds/errata/529-1980.pdf)<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a strapdown sensor for an [inertial navigation system, an attitude reference unit,__________] in an [aircraft, missile,__________] application. The characteristics of the external capture electronics are considered where necessary to define gyro performance. """ #metaKeywords: null #metaDescription: null #shortDescription: "Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95121 …} #channels: Doctrine\ORM\PersistentCollection {#95127 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95123 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95125 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95113 …} -apiLastModifiedAt: DateTime @1754517600 {#95107 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95108 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @349570800 {#95109 : 1981-01-29 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1285797600 {#95110 : 2010-09-30 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @349570800 {#95111 : 1981-01-29 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "529" -bookCollection: "" -pageCount: 24 -documents: Doctrine\ORM\PersistentCollection {#95115 …} -favorites: Doctrine\ORM\PersistentCollection {#95117 …} } ] |
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| Attributes | [ "showFullLabel" => false ] |
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| Component | App\Twig\Components\ProductState {#96404 +product: App\Entity\Product\Product {#95112 #id: 8638 #code: "IEEE00000781" #attributes: Doctrine\ORM\PersistentCollection {#95129 …} #variants: Doctrine\ORM\PersistentCollection {#95131 …} #options: Doctrine\ORM\PersistentCollection {#95135 …} #associations: Doctrine\ORM\PersistentCollection {#95133 …} #createdAt: DateTime @1751037584 {#95105 : 2025-06-27 17:19:44.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95106 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95119 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#96390 #locale: "en_US" #translatable: App\Entity\Product\Product {#95112} #id: 29561 #name: "IEEE 529:1980 (R2010)" #slug: "ieee-529-1980-r2010-ieee00000781-240290" #description: """ New IEEE Standard - Active.<br />\n A specification format guide for the preparation of a rate-integrating gyroscope specification is presented. Recommended procedures for testing a rate-integrating gyroscope are compiled. This standard, when combined with IEEE Std 517-1974 (R1980), defines the requirements and test procedures in terms of characteristics unique to the gyroscope or those applications in which the dynamic angular inputs are significantly greater than the limitations identified in IEEE Std 517. (An errata is available for this standard at http://standards.ieee.org/findstds/errata/529-1980.pdf)<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a strapdown sensor for an [inertial navigation system, an attitude reference unit,__________] in an [aircraft, missile,__________] application. The characteristics of the external capture electronics are considered where necessary to define gyro performance. """ #metaKeywords: null #metaDescription: null #shortDescription: "Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95121 …} #channels: Doctrine\ORM\PersistentCollection {#95127 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95123 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95125 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95113 …} -apiLastModifiedAt: DateTime @1754517600 {#95107 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95108 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @349570800 {#95109 : 1981-01-29 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1285797600 {#95110 : 2010-09-30 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @349570800 {#95111 : 1981-01-29 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "529" -bookCollection: "" -pageCount: 24 -documents: Doctrine\ORM\PersistentCollection {#95115 …} -favorites: Doctrine\ORM\PersistentCollection {#95117 …} } +appearance: "state-active" +labels: [ "Active" ] -stateAttributeCode: "state" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductMostRecent | App\Twig\Components\ProductMostRecent | 82.0 MiB | 0.88 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95112 #id: 8638 #code: "IEEE00000781" #attributes: Doctrine\ORM\PersistentCollection {#95129 …} #variants: Doctrine\ORM\PersistentCollection {#95131 …} #options: Doctrine\ORM\PersistentCollection {#95135 …} #associations: Doctrine\ORM\PersistentCollection {#95133 …} #createdAt: DateTime @1751037584 {#95105 : 2025-06-27 17:19:44.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95106 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95119 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#96390 #locale: "en_US" #translatable: App\Entity\Product\Product {#95112} #id: 29561 #name: "IEEE 529:1980 (R2010)" #slug: "ieee-529-1980-r2010-ieee00000781-240290" #description: """ New IEEE Standard - Active.<br />\n A specification format guide for the preparation of a rate-integrating gyroscope specification is presented. Recommended procedures for testing a rate-integrating gyroscope are compiled. This standard, when combined with IEEE Std 517-1974 (R1980), defines the requirements and test procedures in terms of characteristics unique to the gyroscope or those applications in which the dynamic angular inputs are significantly greater than the limitations identified in IEEE Std 517. (An errata is available for this standard at http://standards.ieee.org/findstds/errata/529-1980.pdf)<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a strapdown sensor for an [inertial navigation system, an attitude reference unit,__________] in an [aircraft, missile,__________] application. The characteristics of the external capture electronics are considered where necessary to define gyro performance. """ #metaKeywords: null #metaDescription: null #shortDescription: "Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95121 …} #channels: Doctrine\ORM\PersistentCollection {#95127 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95123 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95125 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95113 …} -apiLastModifiedAt: DateTime @1754517600 {#95107 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95108 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @349570800 {#95109 : 1981-01-29 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1285797600 {#95110 : 2010-09-30 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @349570800 {#95111 : 1981-01-29 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "529" -bookCollection: "" -pageCount: 24 -documents: Doctrine\ORM\PersistentCollection {#95115 …} -favorites: Doctrine\ORM\PersistentCollection {#95117 …} } ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductMostRecent {#96477 +product: App\Entity\Product\Product {#95112 #id: 8638 #code: "IEEE00000781" #attributes: Doctrine\ORM\PersistentCollection {#95129 …} #variants: Doctrine\ORM\PersistentCollection {#95131 …} #options: Doctrine\ORM\PersistentCollection {#95135 …} #associations: Doctrine\ORM\PersistentCollection {#95133 …} #createdAt: DateTime @1751037584 {#95105 : 2025-06-27 17:19:44.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95106 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95119 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#96390 #locale: "en_US" #translatable: App\Entity\Product\Product {#95112} #id: 29561 #name: "IEEE 529:1980 (R2010)" #slug: "ieee-529-1980-r2010-ieee00000781-240290" #description: """ New IEEE Standard - Active.<br />\n A specification format guide for the preparation of a rate-integrating gyroscope specification is presented. Recommended procedures for testing a rate-integrating gyroscope are compiled. This standard, when combined with IEEE Std 517-1974 (R1980), defines the requirements and test procedures in terms of characteristics unique to the gyroscope or those applications in which the dynamic angular inputs are significantly greater than the limitations identified in IEEE Std 517. (An errata is available for this standard at http://standards.ieee.org/findstds/errata/529-1980.pdf)<br />\n \t\t\t\t<br />\n This specification defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a strapdown sensor for an [inertial navigation system, an attitude reference unit,__________] in an [aircraft, missile,__________] application. The characteristics of the external capture electronics are considered where necessary to define gyro performance. """ #metaKeywords: null #metaDescription: null #shortDescription: "Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95121 …} #channels: Doctrine\ORM\PersistentCollection {#95127 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95123 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95125 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95113 …} -apiLastModifiedAt: DateTime @1754517600 {#95107 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95108 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @349570800 {#95109 : 1981-01-29 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1285797600 {#95110 : 2010-09-30 00:00:00.0 Europe/Paris (+02:00) } -canceledAt: DateTime @349570800 {#95111 : 1981-01-29 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "529" -bookCollection: "" -pageCount: 24 -documents: Doctrine\ORM\PersistentCollection {#95115 …} -favorites: Doctrine\ORM\PersistentCollection {#95117 …} } +label: "Most Recent" +icon: "check-xs" -mostRecentAttributeCode: "most_recent" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductCard | App\Twig\Components\ProductCard | 82.0 MiB | 6.41 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95144 #id: 8874 #code: "IEEE00001200" #attributes: Doctrine\ORM\PersistentCollection {#95161 …} #variants: Doctrine\ORM\PersistentCollection {#95163 …} #options: Doctrine\ORM\PersistentCollection {#95167 …} #associations: Doctrine\ORM\PersistentCollection {#95165 …} #createdAt: DateTime @1751037782 {#95137 : 2025-06-27 17:23:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#95138 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95151 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#96627 #locale: "en_US" #translatable: App\Entity\Product\Product {#95144} #id: 30505 #name: "IEEE 813:1988 (R2011)" #slug: "ieee-813-1988-r2011-ieee00001200-240526" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n A format guide for the preparation of a two-degree-of-freedom dynamically tuned gyro (DTG) specification is given that provides a common ground of terminology and practice for manufacturers and users. A compilation of recommended procedures for testing a DTG is also given. The requirements and test procedures are defined in terms unique to the DTG. They cover applications of the gyro as an angular motion sensor in navigation and control systems. They apply to two modes of use: (1) as a strap-down sensor in operating environments typical of aircraft and missile applications, and (2) as a sensor in gimballed platform applications in which the dynamic angular inputs to which the gyro is subjected are benign relative to the accuracy required. In the case of the strap-down DTG, the characteristics of the external capture loops are considered to the extent necessary to define the gyro performance.<br />\n \t\t\t\t<br />\n This specification defines the requirements for a two-degree-of-freedom dynamically tuned gyro (DTG) to be used as a sensor in a [strapdown, gimballed] [inertial navigation system, attitude reference unit, _______] for use in [an aircraft, a missile, a spacecraft, _______] application. The characteristics of the external capture electronics are considered where necessary to define gyro performance. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Specification Format Guide and Test Procedure for Two-Degree-of-Freedom Dynamically Tuned Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95153 …} #channels: Doctrine\ORM\PersistentCollection {#95159 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95155 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95157 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95145 …} -apiLastModifiedAt: DateTime @1754517600 {#95139 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1648764000 {#95140 : 2022-04-01 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @613000800 {#95141 : 1989-06-05 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: DateTime @1323212400 {#95142 : 2011-12-07 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1648076400 {#95143 : 2022-03-24 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "813" -bookCollection: "" -pageCount: 68 -documents: Doctrine\ORM\PersistentCollection {#95147 …} -favorites: Doctrine\ORM\PersistentCollection {#95149 …} } "layout" => "vertical" "showPrice" => true "showStatusBadges" => true "imageFilter" => "product_listing_thumbnail" "additionalClasses" => "h-100 border-0" "hasStretchedLink" => true "backgroundColor" => "white" "hoverType" => "border-black" ] |
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| Input props | [ "product" => App\Entity\Product\Product {#95237 #id: 8946 #code: "IEEE00001320" #attributes: Doctrine\ORM\PersistentCollection {#95254 …} #variants: Doctrine\ORM\PersistentCollection {#95256 …} #options: Doctrine\ORM\PersistentCollection {#95260 …} #associations: Doctrine\ORM\PersistentCollection {#95258 …} #createdAt: DateTime @1751037842 {#95230 : 2025-06-27 17:24:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754607004 {#95231 : 2025-08-08 00:50:04.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95244 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97274 #locale: "en_US" #translatable: App\Entity\Product\Product {#95237} #id: 30793 #name: "IEEE 952:1997 (R2008)" #slug: "ieee-952-1997-r2008-ieee00001320-240598" #description: """ New IEEE Standard - Superseded.<br />\n Specification and test requirements for a single-axis interferometric fiber optic gyro (IFOG) for use as a sensor in attitude control systems, angular displacement measuring systems, and angular rate measuring systems are defined. A standard specification format guide for the preparation of a single-axis IFOG is provided. A compilation of recommended procedures for testing a fiber optic gyro, derived from those presently used in the industry, is also provided.<br />\n \t\t\t\t<br />\n This standard defines requirements for a single-axis interferometric fiber optic gyro (IFOG), including any necessary electronics, to be used in [an attitude control system, an angular displacement measuring system, an angular rate measuring system, __________]. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Specification Format Guide and Test Procedure for Single-Axis Interferometric Fiber Optic Gyros" -notes: "Superseded" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95246 …} #channels: Doctrine\ORM\PersistentCollection {#95252 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95248 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95250 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95238 …} -apiLastModifiedAt: DateTime @1754517600 {#95232 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1614294000 {#95233 : 2021-02-26 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @880844400 {#95234 : 1997-11-30 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1228863600 {#95235 : 2008-12-10 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @880844400 {#95236 : 1997-11-30 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "952" -bookCollection: "" -pageCount: 84 -documents: Doctrine\ORM\PersistentCollection {#95240 …} -favorites: Doctrine\ORM\PersistentCollection {#95242 …} } ] |
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| ProductCard | App\Twig\Components\ProductCard | 82.0 MiB | 6.31 ms | |
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| Input props | [ "product" => App\Entity\Product\Product {#95268 #id: 9422 #code: "IEEE00002297" #attributes: Doctrine\ORM\PersistentCollection {#95285 …} #variants: Doctrine\ORM\PersistentCollection {#95287 …} #options: Doctrine\ORM\PersistentCollection {#95291 …} #associations: Doctrine\ORM\PersistentCollection {#95289 …} #createdAt: DateTime @1751038251 {#95262 : 2025-06-27 17:30:51.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1753969444 {#95263 : 2025-07-31 15:44:04.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95275 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97503 #locale: "en_US" #translatable: App\Entity\Product\Product {#95268} #id: 32697 #name: "IEEE 1559:2009" #slug: "ieee-1559-2009-ieee00002297-241074" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n Terms and definitions relating to aided and unaided inertial systems for navigation, guidance, orientation, stabilization, and related applications are presented. Usage as understood by the inertial systems community is given preference over general technical usage of the terms herein. The criterion for inclusion of a term and its definition in this document is usefulness as related to inertial systems technology.<br />\n \t\t\t\t<br />\n This standard provides a source of definitions of terminology used in the development, manufacture, and test of aided and unaided inertial systems used for navigation, guidance, orientation, stabilization, and related applications. This is a companion document to IEEE Std 528™.<br />\n There is no consistent definition of terms that have arisen in the evolution of aided and unaided inertial navigation and related systems. This standard is intended to serve as a basic reference for producers and users of such systems, for preparing industry standards, and for the interpretation of published technical reports. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard for Inertial Systems Terminology" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95277 …} #channels: Doctrine\ORM\PersistentCollection {#95283 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95279 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95281 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95269 …} -apiLastModifiedAt: DateTime @1743289200 {#95264 : 2025-03-30 00:00:00.0 Europe/Paris (+01:00) } -lastUpdatedAt: DateTime @1641337200 {#95265 : 2022-01-05 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1251237600 {#95266 : 2009-08-26 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1616626800 {#95267 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "1559" -bookCollection: "" -pageCount: 40 -documents: Doctrine\ORM\PersistentCollection {#95271 …} -favorites: Doctrine\ORM\PersistentCollection {#95273 …} } "layout" => "vertical" "showPrice" => true "showStatusBadges" => true "imageFilter" => "product_listing_thumbnail" "additionalClasses" => "h-100 border-0" "hasStretchedLink" => true "backgroundColor" => "white" "hoverType" => "border-black" ] |
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| Component | App\Twig\Components\ProductCard {#97483 +product: App\Entity\Product\Product {#95268 #id: 9422 #code: "IEEE00002297" #attributes: Doctrine\ORM\PersistentCollection {#95285 …} #variants: Doctrine\ORM\PersistentCollection {#95287 …} #options: Doctrine\ORM\PersistentCollection {#95291 …} #associations: Doctrine\ORM\PersistentCollection {#95289 …} #createdAt: DateTime @1751038251 {#95262 : 2025-06-27 17:30:51.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1753969444 {#95263 : 2025-07-31 15:44:04.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95275 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97503 #locale: "en_US" #translatable: App\Entity\Product\Product {#95268} #id: 32697 #name: "IEEE 1559:2009" #slug: "ieee-1559-2009-ieee00002297-241074" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n Terms and definitions relating to aided and unaided inertial systems for navigation, guidance, orientation, stabilization, and related applications are presented. Usage as understood by the inertial systems community is given preference over general technical usage of the terms herein. The criterion for inclusion of a term and its definition in this document is usefulness as related to inertial systems technology.<br />\n \t\t\t\t<br />\n This standard provides a source of definitions of terminology used in the development, manufacture, and test of aided and unaided inertial systems used for navigation, guidance, orientation, stabilization, and related applications. This is a companion document to IEEE Std 528™.<br />\n There is no consistent definition of terms that have arisen in the evolution of aided and unaided inertial navigation and related systems. This standard is intended to serve as a basic reference for producers and users of such systems, for preparing industry standards, and for the interpretation of published technical reports. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard for Inertial Systems Terminology" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95277 …} #channels: Doctrine\ORM\PersistentCollection {#95283 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95279 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95281 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95269 …} -apiLastModifiedAt: DateTime @1743289200 {#95264 : 2025-03-30 00:00:00.0 Europe/Paris (+01:00) } -lastUpdatedAt: DateTime @1641337200 {#95265 : 2022-01-05 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1251237600 {#95266 : 2009-08-26 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1616626800 {#95267 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "1559" -bookCollection: "" -pageCount: 40 -documents: Doctrine\ORM\PersistentCollection {#95271 …} -favorites: Doctrine\ORM\PersistentCollection {#95273 …} } +layout: "vertical" +showPrice: true +showStatusBadges: true +additionalClasses: "h-100 border-0" +linkLabel: "" +imageFilter: "product_listing_thumbnail" +hasStretchedLink: true +backgroundColor: "white" +hoverType: "border-black" } |
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| ProductState | App\Twig\Components\ProductState | 82.0 MiB | 0.18 ms | |
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| Input props | [ "product" => App\Entity\Product\Product {#95268 #id: 9422 #code: "IEEE00002297" #attributes: Doctrine\ORM\PersistentCollection {#95285 …} #variants: Doctrine\ORM\PersistentCollection {#95287 …} #options: Doctrine\ORM\PersistentCollection {#95291 …} #associations: Doctrine\ORM\PersistentCollection {#95289 …} #createdAt: DateTime @1751038251 {#95262 : 2025-06-27 17:30:51.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1753969444 {#95263 : 2025-07-31 15:44:04.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95275 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97503 #locale: "en_US" #translatable: App\Entity\Product\Product {#95268} #id: 32697 #name: "IEEE 1559:2009" #slug: "ieee-1559-2009-ieee00002297-241074" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n Terms and definitions relating to aided and unaided inertial systems for navigation, guidance, orientation, stabilization, and related applications are presented. Usage as understood by the inertial systems community is given preference over general technical usage of the terms herein. The criterion for inclusion of a term and its definition in this document is usefulness as related to inertial systems technology.<br />\n \t\t\t\t<br />\n This standard provides a source of definitions of terminology used in the development, manufacture, and test of aided and unaided inertial systems used for navigation, guidance, orientation, stabilization, and related applications. This is a companion document to IEEE Std 528™.<br />\n There is no consistent definition of terms that have arisen in the evolution of aided and unaided inertial navigation and related systems. This standard is intended to serve as a basic reference for producers and users of such systems, for preparing industry standards, and for the interpretation of published technical reports. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard for Inertial Systems Terminology" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95277 …} #channels: Doctrine\ORM\PersistentCollection {#95283 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95279 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95281 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95269 …} -apiLastModifiedAt: DateTime @1743289200 {#95264 : 2025-03-30 00:00:00.0 Europe/Paris (+01:00) } -lastUpdatedAt: DateTime @1641337200 {#95265 : 2022-01-05 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1251237600 {#95266 : 2009-08-26 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1616626800 {#95267 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "1559" -bookCollection: "" -pageCount: 40 -documents: Doctrine\ORM\PersistentCollection {#95271 …} -favorites: Doctrine\ORM\PersistentCollection {#95273 …} } ] |
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| Attributes | [ "showFullLabel" => false ] |
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| ProductMostRecent | App\Twig\Components\ProductMostRecent | 82.0 MiB | 0.63 ms | |
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| Input props | [ "product" => App\Entity\Product\Product {#95268 #id: 9422 #code: "IEEE00002297" #attributes: Doctrine\ORM\PersistentCollection {#95285 …} #variants: Doctrine\ORM\PersistentCollection {#95287 …} #options: Doctrine\ORM\PersistentCollection {#95291 …} #associations: Doctrine\ORM\PersistentCollection {#95289 …} #createdAt: DateTime @1751038251 {#95262 : 2025-06-27 17:30:51.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1753969444 {#95263 : 2025-07-31 15:44:04.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95275 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97503 #locale: "en_US" #translatable: App\Entity\Product\Product {#95268} #id: 32697 #name: "IEEE 1559:2009" #slug: "ieee-1559-2009-ieee00002297-241074" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n Terms and definitions relating to aided and unaided inertial systems for navigation, guidance, orientation, stabilization, and related applications are presented. Usage as understood by the inertial systems community is given preference over general technical usage of the terms herein. The criterion for inclusion of a term and its definition in this document is usefulness as related to inertial systems technology.<br />\n \t\t\t\t<br />\n This standard provides a source of definitions of terminology used in the development, manufacture, and test of aided and unaided inertial systems used for navigation, guidance, orientation, stabilization, and related applications. This is a companion document to IEEE Std 528™.<br />\n There is no consistent definition of terms that have arisen in the evolution of aided and unaided inertial navigation and related systems. This standard is intended to serve as a basic reference for producers and users of such systems, for preparing industry standards, and for the interpretation of published technical reports. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard for Inertial Systems Terminology" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95277 …} #channels: Doctrine\ORM\PersistentCollection {#95283 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95279 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95281 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95269 …} -apiLastModifiedAt: DateTime @1743289200 {#95264 : 2025-03-30 00:00:00.0 Europe/Paris (+01:00) } -lastUpdatedAt: DateTime @1641337200 {#95265 : 2022-01-05 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1251237600 {#95266 : 2009-08-26 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1616626800 {#95267 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "1559" -bookCollection: "" -pageCount: 40 -documents: Doctrine\ORM\PersistentCollection {#95271 …} -favorites: Doctrine\ORM\PersistentCollection {#95273 …} } ] |
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| ProductCard | App\Twig\Components\ProductCard | 82.0 MiB | 6.23 ms | |
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| Input props | [ "product" => App\Entity\Product\Product {#95299 #id: 10016 #code: "IEEE00003449" #attributes: Doctrine\ORM\PersistentCollection {#95316 …} #variants: Doctrine\ORM\PersistentCollection {#95318 …} #options: Doctrine\ORM\PersistentCollection {#95322 …} #associations: Doctrine\ORM\PersistentCollection {#95320 …} #createdAt: DateTime @1751038748 {#95293 : 2025-06-27 17:39:08.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754607611 {#95294 : 2025-08-08 01:00:11.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95306 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97733 #locale: "en_US" #translatable: App\Entity\Product\Product {#95299} #id: 35073 #name: "IEEE 836:2009" #slug: "ieee-836-2009-ieee00003449-241668" #description: """ Revision Standard - Inactive-Reserved.<br />\n This recommended practice describes the conduct and analysis of precision tests that are to be performed on linear accelerometers using centrifuge techniques. The term "precision," in this context, refers to tests that are conducted to evaluate accelerometer parameters, as opposed to those conducted to establish environmental survivability only. Evaluation may take the form of determining the coefficients of the accelerometer's model equation, except for bias and scale factor, which are most accurately determined by static multi-position tests. Alternatively, evaluation may only establish that the accelerometer output complies with specific error limit criteria.<br />\n \t\t\t\t<br />\n This recommended practice describes the conduct and analysis of precision tests that are to be performed on linear accelerometers using centrifuge techniques. The term "precision," in this context, refers to tests that are conducted to evaluate accelerometer parameters, as opposed to tests conducted to establish environmental survivability only. Evaluation may take the form of determining the coefficients of the accelerometer's model equation, except for bias and scale factor, which are most accurately determined by static multiposition tests. Alternatively, evaluation may establish only that the accelerometer output complies with specific error limit criteria.<br />\n The principal error sources encountered during precision centrifuge testing of linear accelerometers are described, along with the test practices and data reduction techniques that have been found most efficient in minimizing or compensating for them. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Recommended Practice for Precision Centrifuge Testing of Linear Accelerometers" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95308 …} #channels: Doctrine\ORM\PersistentCollection {#95314 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95310 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95312 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95300 …} -apiLastModifiedAt: DateTime @1754517600 {#95295 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1701730800 {#95296 : 2023-12-05 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1253138400 {#95297 : 2009-09-17 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1583362800 {#95298 : 2020-03-05 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "836" -bookCollection: "" -pageCount: 152 -documents: Doctrine\ORM\PersistentCollection {#95302 …} -favorites: Doctrine\ORM\PersistentCollection {#95304 …} } "layout" => "vertical" "showPrice" => true "showStatusBadges" => true "imageFilter" => "product_listing_thumbnail" "additionalClasses" => "h-100 border-0" "hasStretchedLink" => true "backgroundColor" => "secondary-lighter" "hoverType" => "border-black" ] |
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| Component | App\Twig\Components\ProductCard {#97713 +product: App\Entity\Product\Product {#95299 #id: 10016 #code: "IEEE00003449" #attributes: Doctrine\ORM\PersistentCollection {#95316 …} #variants: Doctrine\ORM\PersistentCollection {#95318 …} #options: Doctrine\ORM\PersistentCollection {#95322 …} #associations: Doctrine\ORM\PersistentCollection {#95320 …} #createdAt: DateTime @1751038748 {#95293 : 2025-06-27 17:39:08.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754607611 {#95294 : 2025-08-08 01:00:11.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95306 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97733 #locale: "en_US" #translatable: App\Entity\Product\Product {#95299} #id: 35073 #name: "IEEE 836:2009" #slug: "ieee-836-2009-ieee00003449-241668" #description: """ Revision Standard - Inactive-Reserved.<br />\n This recommended practice describes the conduct and analysis of precision tests that are to be performed on linear accelerometers using centrifuge techniques. The term "precision," in this context, refers to tests that are conducted to evaluate accelerometer parameters, as opposed to those conducted to establish environmental survivability only. Evaluation may take the form of determining the coefficients of the accelerometer's model equation, except for bias and scale factor, which are most accurately determined by static multi-position tests. Alternatively, evaluation may only establish that the accelerometer output complies with specific error limit criteria.<br />\n \t\t\t\t<br />\n This recommended practice describes the conduct and analysis of precision tests that are to be performed on linear accelerometers using centrifuge techniques. The term "precision," in this context, refers to tests that are conducted to evaluate accelerometer parameters, as opposed to tests conducted to establish environmental survivability only. Evaluation may take the form of determining the coefficients of the accelerometer's model equation, except for bias and scale factor, which are most accurately determined by static multiposition tests. Alternatively, evaluation may establish only that the accelerometer output complies with specific error limit criteria.<br />\n The principal error sources encountered during precision centrifuge testing of linear accelerometers are described, along with the test practices and data reduction techniques that have been found most efficient in minimizing or compensating for them. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Recommended Practice for Precision Centrifuge Testing of Linear Accelerometers" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95308 …} #channels: Doctrine\ORM\PersistentCollection {#95314 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95310 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95312 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95300 …} -apiLastModifiedAt: DateTime @1754517600 {#95295 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1701730800 {#95296 : 2023-12-05 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1253138400 {#95297 : 2009-09-17 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1583362800 {#95298 : 2020-03-05 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "836" -bookCollection: "" -pageCount: 152 -documents: Doctrine\ORM\PersistentCollection {#95302 …} -favorites: Doctrine\ORM\PersistentCollection {#95304 …} } +layout: "vertical" +showPrice: true +showStatusBadges: true +additionalClasses: "h-100 border-0" +linkLabel: "" +imageFilter: "product_listing_thumbnail" +hasStretchedLink: true +backgroundColor: "secondary-lighter" +hoverType: "border-black" } |
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| ProductState | App\Twig\Components\ProductState | 82.0 MiB | 0.19 ms | |
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| Input props | [ "product" => App\Entity\Product\Product {#95299 #id: 10016 #code: "IEEE00003449" #attributes: Doctrine\ORM\PersistentCollection {#95316 …} #variants: Doctrine\ORM\PersistentCollection {#95318 …} #options: Doctrine\ORM\PersistentCollection {#95322 …} #associations: Doctrine\ORM\PersistentCollection {#95320 …} #createdAt: DateTime @1751038748 {#95293 : 2025-06-27 17:39:08.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754607611 {#95294 : 2025-08-08 01:00:11.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95306 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97733 #locale: "en_US" #translatable: App\Entity\Product\Product {#95299} #id: 35073 #name: "IEEE 836:2009" #slug: "ieee-836-2009-ieee00003449-241668" #description: """ Revision Standard - Inactive-Reserved.<br />\n This recommended practice describes the conduct and analysis of precision tests that are to be performed on linear accelerometers using centrifuge techniques. The term "precision," in this context, refers to tests that are conducted to evaluate accelerometer parameters, as opposed to those conducted to establish environmental survivability only. Evaluation may take the form of determining the coefficients of the accelerometer's model equation, except for bias and scale factor, which are most accurately determined by static multi-position tests. Alternatively, evaluation may only establish that the accelerometer output complies with specific error limit criteria.<br />\n \t\t\t\t<br />\n This recommended practice describes the conduct and analysis of precision tests that are to be performed on linear accelerometers using centrifuge techniques. The term "precision," in this context, refers to tests that are conducted to evaluate accelerometer parameters, as opposed to tests conducted to establish environmental survivability only. Evaluation may take the form of determining the coefficients of the accelerometer's model equation, except for bias and scale factor, which are most accurately determined by static multiposition tests. Alternatively, evaluation may establish only that the accelerometer output complies with specific error limit criteria.<br />\n The principal error sources encountered during precision centrifuge testing of linear accelerometers are described, along with the test practices and data reduction techniques that have been found most efficient in minimizing or compensating for them. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Recommended Practice for Precision Centrifuge Testing of Linear Accelerometers" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95308 …} #channels: Doctrine\ORM\PersistentCollection {#95314 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95310 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95312 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95300 …} -apiLastModifiedAt: DateTime @1754517600 {#95295 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1701730800 {#95296 : 2023-12-05 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1253138400 {#95297 : 2009-09-17 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1583362800 {#95298 : 2020-03-05 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "836" -bookCollection: "" -pageCount: 152 -documents: Doctrine\ORM\PersistentCollection {#95302 …} -favorites: Doctrine\ORM\PersistentCollection {#95304 …} } ] |
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| Component | App\Twig\Components\ProductState {#97747 +product: App\Entity\Product\Product {#95299 #id: 10016 #code: "IEEE00003449" #attributes: Doctrine\ORM\PersistentCollection {#95316 …} #variants: Doctrine\ORM\PersistentCollection {#95318 …} #options: Doctrine\ORM\PersistentCollection {#95322 …} #associations: Doctrine\ORM\PersistentCollection {#95320 …} #createdAt: DateTime @1751038748 {#95293 : 2025-06-27 17:39:08.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754607611 {#95294 : 2025-08-08 01:00:11.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95306 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97733 #locale: "en_US" #translatable: App\Entity\Product\Product {#95299} #id: 35073 #name: "IEEE 836:2009" #slug: "ieee-836-2009-ieee00003449-241668" #description: """ Revision Standard - Inactive-Reserved.<br />\n This recommended practice describes the conduct and analysis of precision tests that are to be performed on linear accelerometers using centrifuge techniques. The term "precision," in this context, refers to tests that are conducted to evaluate accelerometer parameters, as opposed to those conducted to establish environmental survivability only. Evaluation may take the form of determining the coefficients of the accelerometer's model equation, except for bias and scale factor, which are most accurately determined by static multi-position tests. Alternatively, evaluation may only establish that the accelerometer output complies with specific error limit criteria.<br />\n \t\t\t\t<br />\n This recommended practice describes the conduct and analysis of precision tests that are to be performed on linear accelerometers using centrifuge techniques. The term "precision," in this context, refers to tests that are conducted to evaluate accelerometer parameters, as opposed to tests conducted to establish environmental survivability only. Evaluation may take the form of determining the coefficients of the accelerometer's model equation, except for bias and scale factor, which are most accurately determined by static multiposition tests. Alternatively, evaluation may establish only that the accelerometer output complies with specific error limit criteria.<br />\n The principal error sources encountered during precision centrifuge testing of linear accelerometers are described, along with the test practices and data reduction techniques that have been found most efficient in minimizing or compensating for them. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Recommended Practice for Precision Centrifuge Testing of Linear Accelerometers" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95308 …} #channels: Doctrine\ORM\PersistentCollection {#95314 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95310 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95312 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95300 …} -apiLastModifiedAt: DateTime @1754517600 {#95295 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1701730800 {#95296 : 2023-12-05 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1253138400 {#95297 : 2009-09-17 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1583362800 {#95298 : 2020-03-05 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "836" -bookCollection: "" -pageCount: 152 -documents: Doctrine\ORM\PersistentCollection {#95302 …} -favorites: Doctrine\ORM\PersistentCollection {#95304 …} } +appearance: "state-withdrawn" +labels: [ "Withdrawn" ] -stateAttributeCode: "state" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductMostRecent | App\Twig\Components\ProductMostRecent | 82.0 MiB | 0.63 ms | |
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| Input props | [ "product" => App\Entity\Product\Product {#95299 #id: 10016 #code: "IEEE00003449" #attributes: Doctrine\ORM\PersistentCollection {#95316 …} #variants: Doctrine\ORM\PersistentCollection {#95318 …} #options: Doctrine\ORM\PersistentCollection {#95322 …} #associations: Doctrine\ORM\PersistentCollection {#95320 …} #createdAt: DateTime @1751038748 {#95293 : 2025-06-27 17:39:08.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754607611 {#95294 : 2025-08-08 01:00:11.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95306 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97733 #locale: "en_US" #translatable: App\Entity\Product\Product {#95299} #id: 35073 #name: "IEEE 836:2009" #slug: "ieee-836-2009-ieee00003449-241668" #description: """ Revision Standard - Inactive-Reserved.<br />\n This recommended practice describes the conduct and analysis of precision tests that are to be performed on linear accelerometers using centrifuge techniques. The term "precision," in this context, refers to tests that are conducted to evaluate accelerometer parameters, as opposed to those conducted to establish environmental survivability only. Evaluation may take the form of determining the coefficients of the accelerometer's model equation, except for bias and scale factor, which are most accurately determined by static multi-position tests. Alternatively, evaluation may only establish that the accelerometer output complies with specific error limit criteria.<br />\n \t\t\t\t<br />\n This recommended practice describes the conduct and analysis of precision tests that are to be performed on linear accelerometers using centrifuge techniques. The term "precision," in this context, refers to tests that are conducted to evaluate accelerometer parameters, as opposed to tests conducted to establish environmental survivability only. Evaluation may take the form of determining the coefficients of the accelerometer's model equation, except for bias and scale factor, which are most accurately determined by static multiposition tests. Alternatively, evaluation may establish only that the accelerometer output complies with specific error limit criteria.<br />\n The principal error sources encountered during precision centrifuge testing of linear accelerometers are described, along with the test practices and data reduction techniques that have been found most efficient in minimizing or compensating for them. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Recommended Practice for Precision Centrifuge Testing of Linear Accelerometers" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95308 …} #channels: Doctrine\ORM\PersistentCollection {#95314 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95310 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95312 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95300 …} -apiLastModifiedAt: DateTime @1754517600 {#95295 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1701730800 {#95296 : 2023-12-05 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1253138400 {#95297 : 2009-09-17 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1583362800 {#95298 : 2020-03-05 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "836" -bookCollection: "" -pageCount: 152 -documents: Doctrine\ORM\PersistentCollection {#95302 …} -favorites: Doctrine\ORM\PersistentCollection {#95304 …} } ] |
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| Component | App\Twig\Components\ProductMostRecent {#97821 +product: App\Entity\Product\Product {#95299 #id: 10016 #code: "IEEE00003449" #attributes: Doctrine\ORM\PersistentCollection {#95316 …} #variants: Doctrine\ORM\PersistentCollection {#95318 …} #options: Doctrine\ORM\PersistentCollection {#95322 …} #associations: Doctrine\ORM\PersistentCollection {#95320 …} #createdAt: DateTime @1751038748 {#95293 : 2025-06-27 17:39:08.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754607611 {#95294 : 2025-08-08 01:00:11.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95306 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97733 #locale: "en_US" #translatable: App\Entity\Product\Product {#95299} #id: 35073 #name: "IEEE 836:2009" #slug: "ieee-836-2009-ieee00003449-241668" #description: """ Revision Standard - Inactive-Reserved.<br />\n This recommended practice describes the conduct and analysis of precision tests that are to be performed on linear accelerometers using centrifuge techniques. The term "precision," in this context, refers to tests that are conducted to evaluate accelerometer parameters, as opposed to those conducted to establish environmental survivability only. Evaluation may take the form of determining the coefficients of the accelerometer's model equation, except for bias and scale factor, which are most accurately determined by static multi-position tests. Alternatively, evaluation may only establish that the accelerometer output complies with specific error limit criteria.<br />\n \t\t\t\t<br />\n This recommended practice describes the conduct and analysis of precision tests that are to be performed on linear accelerometers using centrifuge techniques. The term "precision," in this context, refers to tests that are conducted to evaluate accelerometer parameters, as opposed to tests conducted to establish environmental survivability only. Evaluation may take the form of determining the coefficients of the accelerometer's model equation, except for bias and scale factor, which are most accurately determined by static multiposition tests. Alternatively, evaluation may establish only that the accelerometer output complies with specific error limit criteria.<br />\n The principal error sources encountered during precision centrifuge testing of linear accelerometers are described, along with the test practices and data reduction techniques that have been found most efficient in minimizing or compensating for them. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Recommended Practice for Precision Centrifuge Testing of Linear Accelerometers" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95308 …} #channels: Doctrine\ORM\PersistentCollection {#95314 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95310 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95312 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95300 …} -apiLastModifiedAt: DateTime @1754517600 {#95295 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1701730800 {#95296 : 2023-12-05 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1253138400 {#95297 : 2009-09-17 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1583362800 {#95298 : 2020-03-05 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "836" -bookCollection: "" -pageCount: 152 -documents: Doctrine\ORM\PersistentCollection {#95302 …} -favorites: Doctrine\ORM\PersistentCollection {#95304 …} } +label: "Most Recent" +icon: "check-xs" -mostRecentAttributeCode: "most_recent" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductCard | App\Twig\Components\ProductCard | 82.0 MiB | 6.16 ms | |
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| Input props | [ "product" => App\Entity\Product\Product {#95331 #id: 10046 #code: "IEEE00003519" #attributes: Doctrine\ORM\PersistentCollection {#95348 …} #variants: Doctrine\ORM\PersistentCollection {#95350 …} #options: Doctrine\ORM\PersistentCollection {#95354 …} #associations: Doctrine\ORM\PersistentCollection {#95352 …} #createdAt: DateTime @1751038773 {#95324 : 2025-06-27 17:39:33.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754608190 {#95325 : 2025-08-08 01:09:50.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95338 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97963 #locale: "en_US" #translatable: App\Entity\Product\Product {#95331} #id: 35193 #name: "IEEE 1431:2004 (R2010)" #slug: "ieee-1431-2004-r2010-ieee00003519-241698" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n <br />\n \t\t\t\t<br />\n Specification and test requirements for a single-axis Coriolis vibratory gyro (CVG) for use as a sensor in attitude control systems, angular displacement measuring systems, and angular rate measuring systems are defined. A stadard specification format guide for the preparation of a single-axis CVG is provided. A complilation of recommended procedures for testing a CVG, derived from those presently used in the industry, is also provided. Informative annexes cover CVG design features and theoretical principles of operation.<br />\n This standard is provided as a guide for the preparation of Coriolis vibratory gyro (CVG) specification and test procedures. The CVG is a device which measures inertial angular rate through the Coriolis force produced from a vibrating mass in a non-inertial reference frame. This gyro type encompasses low cost Micro-Electro-Mechanical-Systems (MEMS) devices on silicon or quartz chips and also inertial navigation grade vibrating shell gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95340 …} #channels: Doctrine\ORM\PersistentCollection {#95346 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95342 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95344 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95332 …} -apiLastModifiedAt: DateTime @1754517600 {#95326 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618437600 {#95327 : 2021-04-15 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1103497200 {#95328 : 2004-12-20 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1269471600 {#95329 : 2010-03-25 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1616626800 {#95330 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "1431" -bookCollection: "" -pageCount: 78 -documents: Doctrine\ORM\PersistentCollection {#95334 …} -favorites: Doctrine\ORM\PersistentCollection {#95336 …} } "layout" => "vertical" "showPrice" => true "showStatusBadges" => true "imageFilter" => "product_listing_thumbnail" "additionalClasses" => "h-100 border-0" "hasStretchedLink" => true "backgroundColor" => "white" "hoverType" => "border-black" ] |
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| Component | App\Twig\Components\ProductCard {#97943 +product: App\Entity\Product\Product {#95331 #id: 10046 #code: "IEEE00003519" #attributes: Doctrine\ORM\PersistentCollection {#95348 …} #variants: Doctrine\ORM\PersistentCollection {#95350 …} #options: Doctrine\ORM\PersistentCollection {#95354 …} #associations: Doctrine\ORM\PersistentCollection {#95352 …} #createdAt: DateTime @1751038773 {#95324 : 2025-06-27 17:39:33.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754608190 {#95325 : 2025-08-08 01:09:50.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95338 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97963 #locale: "en_US" #translatable: App\Entity\Product\Product {#95331} #id: 35193 #name: "IEEE 1431:2004 (R2010)" #slug: "ieee-1431-2004-r2010-ieee00003519-241698" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n <br />\n \t\t\t\t<br />\n Specification and test requirements for a single-axis Coriolis vibratory gyro (CVG) for use as a sensor in attitude control systems, angular displacement measuring systems, and angular rate measuring systems are defined. A stadard specification format guide for the preparation of a single-axis CVG is provided. A complilation of recommended procedures for testing a CVG, derived from those presently used in the industry, is also provided. Informative annexes cover CVG design features and theoretical principles of operation.<br />\n This standard is provided as a guide for the preparation of Coriolis vibratory gyro (CVG) specification and test procedures. The CVG is a device which measures inertial angular rate through the Coriolis force produced from a vibrating mass in a non-inertial reference frame. This gyro type encompasses low cost Micro-Electro-Mechanical-Systems (MEMS) devices on silicon or quartz chips and also inertial navigation grade vibrating shell gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95340 …} #channels: Doctrine\ORM\PersistentCollection {#95346 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95342 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95344 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95332 …} -apiLastModifiedAt: DateTime @1754517600 {#95326 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618437600 {#95327 : 2021-04-15 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1103497200 {#95328 : 2004-12-20 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1269471600 {#95329 : 2010-03-25 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1616626800 {#95330 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "1431" -bookCollection: "" -pageCount: 78 -documents: Doctrine\ORM\PersistentCollection {#95334 …} -favorites: Doctrine\ORM\PersistentCollection {#95336 …} } +layout: "vertical" +showPrice: true +showStatusBadges: true +additionalClasses: "h-100 border-0" +linkLabel: "" +imageFilter: "product_listing_thumbnail" +hasStretchedLink: true +backgroundColor: "white" +hoverType: "border-black" } |
|||
| ProductState | App\Twig\Components\ProductState | 82.0 MiB | 0.19 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95331 #id: 10046 #code: "IEEE00003519" #attributes: Doctrine\ORM\PersistentCollection {#95348 …} #variants: Doctrine\ORM\PersistentCollection {#95350 …} #options: Doctrine\ORM\PersistentCollection {#95354 …} #associations: Doctrine\ORM\PersistentCollection {#95352 …} #createdAt: DateTime @1751038773 {#95324 : 2025-06-27 17:39:33.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754608190 {#95325 : 2025-08-08 01:09:50.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95338 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97963 #locale: "en_US" #translatable: App\Entity\Product\Product {#95331} #id: 35193 #name: "IEEE 1431:2004 (R2010)" #slug: "ieee-1431-2004-r2010-ieee00003519-241698" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n <br />\n \t\t\t\t<br />\n Specification and test requirements for a single-axis Coriolis vibratory gyro (CVG) for use as a sensor in attitude control systems, angular displacement measuring systems, and angular rate measuring systems are defined. A stadard specification format guide for the preparation of a single-axis CVG is provided. A complilation of recommended procedures for testing a CVG, derived from those presently used in the industry, is also provided. Informative annexes cover CVG design features and theoretical principles of operation.<br />\n This standard is provided as a guide for the preparation of Coriolis vibratory gyro (CVG) specification and test procedures. The CVG is a device which measures inertial angular rate through the Coriolis force produced from a vibrating mass in a non-inertial reference frame. This gyro type encompasses low cost Micro-Electro-Mechanical-Systems (MEMS) devices on silicon or quartz chips and also inertial navigation grade vibrating shell gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95340 …} #channels: Doctrine\ORM\PersistentCollection {#95346 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95342 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95344 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95332 …} -apiLastModifiedAt: DateTime @1754517600 {#95326 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618437600 {#95327 : 2021-04-15 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1103497200 {#95328 : 2004-12-20 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1269471600 {#95329 : 2010-03-25 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1616626800 {#95330 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "1431" -bookCollection: "" -pageCount: 78 -documents: Doctrine\ORM\PersistentCollection {#95334 …} -favorites: Doctrine\ORM\PersistentCollection {#95336 …} } ] |
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| Attributes | [ "showFullLabel" => false ] |
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| Component | App\Twig\Components\ProductState {#97970 +product: App\Entity\Product\Product {#95331 #id: 10046 #code: "IEEE00003519" #attributes: Doctrine\ORM\PersistentCollection {#95348 …} #variants: Doctrine\ORM\PersistentCollection {#95350 …} #options: Doctrine\ORM\PersistentCollection {#95354 …} #associations: Doctrine\ORM\PersistentCollection {#95352 …} #createdAt: DateTime @1751038773 {#95324 : 2025-06-27 17:39:33.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754608190 {#95325 : 2025-08-08 01:09:50.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95338 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97963 #locale: "en_US" #translatable: App\Entity\Product\Product {#95331} #id: 35193 #name: "IEEE 1431:2004 (R2010)" #slug: "ieee-1431-2004-r2010-ieee00003519-241698" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n <br />\n \t\t\t\t<br />\n Specification and test requirements for a single-axis Coriolis vibratory gyro (CVG) for use as a sensor in attitude control systems, angular displacement measuring systems, and angular rate measuring systems are defined. A stadard specification format guide for the preparation of a single-axis CVG is provided. A complilation of recommended procedures for testing a CVG, derived from those presently used in the industry, is also provided. Informative annexes cover CVG design features and theoretical principles of operation.<br />\n This standard is provided as a guide for the preparation of Coriolis vibratory gyro (CVG) specification and test procedures. The CVG is a device which measures inertial angular rate through the Coriolis force produced from a vibrating mass in a non-inertial reference frame. This gyro type encompasses low cost Micro-Electro-Mechanical-Systems (MEMS) devices on silicon or quartz chips and also inertial navigation grade vibrating shell gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95340 …} #channels: Doctrine\ORM\PersistentCollection {#95346 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95342 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95344 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95332 …} -apiLastModifiedAt: DateTime @1754517600 {#95326 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618437600 {#95327 : 2021-04-15 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1103497200 {#95328 : 2004-12-20 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1269471600 {#95329 : 2010-03-25 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1616626800 {#95330 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "1431" -bookCollection: "" -pageCount: 78 -documents: Doctrine\ORM\PersistentCollection {#95334 …} -favorites: Doctrine\ORM\PersistentCollection {#95336 …} } +appearance: "state-withdrawn" +labels: [ "Withdrawn" ] -stateAttributeCode: "state" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
|||
| ProductMostRecent | App\Twig\Components\ProductMostRecent | 82.0 MiB | 0.63 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95331 #id: 10046 #code: "IEEE00003519" #attributes: Doctrine\ORM\PersistentCollection {#95348 …} #variants: Doctrine\ORM\PersistentCollection {#95350 …} #options: Doctrine\ORM\PersistentCollection {#95354 …} #associations: Doctrine\ORM\PersistentCollection {#95352 …} #createdAt: DateTime @1751038773 {#95324 : 2025-06-27 17:39:33.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754608190 {#95325 : 2025-08-08 01:09:50.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95338 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97963 #locale: "en_US" #translatable: App\Entity\Product\Product {#95331} #id: 35193 #name: "IEEE 1431:2004 (R2010)" #slug: "ieee-1431-2004-r2010-ieee00003519-241698" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n <br />\n \t\t\t\t<br />\n Specification and test requirements for a single-axis Coriolis vibratory gyro (CVG) for use as a sensor in attitude control systems, angular displacement measuring systems, and angular rate measuring systems are defined. A stadard specification format guide for the preparation of a single-axis CVG is provided. A complilation of recommended procedures for testing a CVG, derived from those presently used in the industry, is also provided. Informative annexes cover CVG design features and theoretical principles of operation.<br />\n This standard is provided as a guide for the preparation of Coriolis vibratory gyro (CVG) specification and test procedures. The CVG is a device which measures inertial angular rate through the Coriolis force produced from a vibrating mass in a non-inertial reference frame. This gyro type encompasses low cost Micro-Electro-Mechanical-Systems (MEMS) devices on silicon or quartz chips and also inertial navigation grade vibrating shell gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95340 …} #channels: Doctrine\ORM\PersistentCollection {#95346 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95342 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95344 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95332 …} -apiLastModifiedAt: DateTime @1754517600 {#95326 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618437600 {#95327 : 2021-04-15 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1103497200 {#95328 : 2004-12-20 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1269471600 {#95329 : 2010-03-25 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1616626800 {#95330 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "1431" -bookCollection: "" -pageCount: 78 -documents: Doctrine\ORM\PersistentCollection {#95334 …} -favorites: Doctrine\ORM\PersistentCollection {#95336 …} } ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductMostRecent {#98047 +product: App\Entity\Product\Product {#95331 #id: 10046 #code: "IEEE00003519" #attributes: Doctrine\ORM\PersistentCollection {#95348 …} #variants: Doctrine\ORM\PersistentCollection {#95350 …} #options: Doctrine\ORM\PersistentCollection {#95354 …} #associations: Doctrine\ORM\PersistentCollection {#95352 …} #createdAt: DateTime @1751038773 {#95324 : 2025-06-27 17:39:33.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754608190 {#95325 : 2025-08-08 01:09:50.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95338 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#97963 #locale: "en_US" #translatable: App\Entity\Product\Product {#95331} #id: 35193 #name: "IEEE 1431:2004 (R2010)" #slug: "ieee-1431-2004-r2010-ieee00003519-241698" #description: """ New IEEE Standard - Inactive-Reserved.<br />\n <br />\n \t\t\t\t<br />\n Specification and test requirements for a single-axis Coriolis vibratory gyro (CVG) for use as a sensor in attitude control systems, angular displacement measuring systems, and angular rate measuring systems are defined. A stadard specification format guide for the preparation of a single-axis CVG is provided. A complilation of recommended procedures for testing a CVG, derived from those presently used in the industry, is also provided. Informative annexes cover CVG design features and theoretical principles of operation.<br />\n This standard is provided as a guide for the preparation of Coriolis vibratory gyro (CVG) specification and test procedures. The CVG is a device which measures inertial angular rate through the Coriolis force produced from a vibrating mass in a non-inertial reference frame. This gyro type encompasses low cost Micro-Electro-Mechanical-Systems (MEMS) devices on silicon or quartz chips and also inertial navigation grade vibrating shell gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95340 …} #channels: Doctrine\ORM\PersistentCollection {#95346 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95342 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95344 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95332 …} -apiLastModifiedAt: DateTime @1754517600 {#95326 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618437600 {#95327 : 2021-04-15 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1103497200 {#95328 : 2004-12-20 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: DateTime @1269471600 {#95329 : 2010-03-25 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1616626800 {#95330 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "1431" -bookCollection: "" -pageCount: 78 -documents: Doctrine\ORM\PersistentCollection {#95334 …} -favorites: Doctrine\ORM\PersistentCollection {#95336 …} } +label: "Most Recent" +icon: "check-xs" -mostRecentAttributeCode: "most_recent" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductCard | App\Twig\Components\ProductCard | 82.0 MiB | 6.13 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95363 #id: 10311 #code: "IEEE00004143" #attributes: Doctrine\ORM\PersistentCollection {#95380 …} #variants: Doctrine\ORM\PersistentCollection {#95382 …} #options: Doctrine\ORM\PersistentCollection {#95386 …} #associations: Doctrine\ORM\PersistentCollection {#95384 …} #createdAt: DateTime @1751038981 {#95356 : 2025-06-27 17:43:01.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754607611 {#95357 : 2025-08-08 01:00:11.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95370 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98172 #locale: "en_US" #translatable: App\Entity\Product\Product {#95363} #id: 36253 #name: "IEEE 1431-2004/Cor 1:2008 (R2010)" #slug: "ieee-1431-2004-cor-1-2008-r2010-ieee00004143-241963" #description: """ Corrigendum Standard - Inactive-Reserved.<br />\n Corrigendum to IEEE Std 1431-2004.<br />\n \t\t\t\t<br />\n Correction of labeling errors on several figures.<br />\n Establish consistent use of symbols and terminology. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros - Corrigendum 1" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95372 …} #channels: Doctrine\ORM\PersistentCollection {#95378 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95374 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95376 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95364 …} -apiLastModifiedAt: DateTime @1754517600 {#95358 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618524000 {#95359 : 2021-04-16 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1223503200 {#95360 : 2008-10-09 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: DateTime @1269471600 {#95361 : 2010-03-25 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1616626800 {#95362 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "1431" -bookCollection: "" -pageCount: 79 -documents: Doctrine\ORM\PersistentCollection {#95366 …} -favorites: Doctrine\ORM\PersistentCollection {#95368 …} } "layout" => "vertical" "showPrice" => true "showStatusBadges" => true "imageFilter" => "product_listing_thumbnail" "additionalClasses" => "h-100 border-0" "hasStretchedLink" => true "backgroundColor" => "secondary-lighter" "hoverType" => "border-black" ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductCard {#98152 +product: App\Entity\Product\Product {#95363 #id: 10311 #code: "IEEE00004143" #attributes: Doctrine\ORM\PersistentCollection {#95380 …} #variants: Doctrine\ORM\PersistentCollection {#95382 …} #options: Doctrine\ORM\PersistentCollection {#95386 …} #associations: Doctrine\ORM\PersistentCollection {#95384 …} #createdAt: DateTime @1751038981 {#95356 : 2025-06-27 17:43:01.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754607611 {#95357 : 2025-08-08 01:00:11.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95370 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98172 #locale: "en_US" #translatable: App\Entity\Product\Product {#95363} #id: 36253 #name: "IEEE 1431-2004/Cor 1:2008 (R2010)" #slug: "ieee-1431-2004-cor-1-2008-r2010-ieee00004143-241963" #description: """ Corrigendum Standard - Inactive-Reserved.<br />\n Corrigendum to IEEE Std 1431-2004.<br />\n \t\t\t\t<br />\n Correction of labeling errors on several figures.<br />\n Establish consistent use of symbols and terminology. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros - Corrigendum 1" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95372 …} #channels: Doctrine\ORM\PersistentCollection {#95378 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95374 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95376 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95364 …} -apiLastModifiedAt: DateTime @1754517600 {#95358 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618524000 {#95359 : 2021-04-16 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1223503200 {#95360 : 2008-10-09 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: DateTime @1269471600 {#95361 : 2010-03-25 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1616626800 {#95362 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "1431" -bookCollection: "" -pageCount: 79 -documents: Doctrine\ORM\PersistentCollection {#95366 …} -favorites: Doctrine\ORM\PersistentCollection {#95368 …} } +layout: "vertical" +showPrice: true +showStatusBadges: true +additionalClasses: "h-100 border-0" +linkLabel: "" +imageFilter: "product_listing_thumbnail" +hasStretchedLink: true +backgroundColor: "secondary-lighter" +hoverType: "border-black" } |
|||
| ProductState | App\Twig\Components\ProductState | 82.0 MiB | 0.19 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95363 #id: 10311 #code: "IEEE00004143" #attributes: Doctrine\ORM\PersistentCollection {#95380 …} #variants: Doctrine\ORM\PersistentCollection {#95382 …} #options: Doctrine\ORM\PersistentCollection {#95386 …} #associations: Doctrine\ORM\PersistentCollection {#95384 …} #createdAt: DateTime @1751038981 {#95356 : 2025-06-27 17:43:01.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754607611 {#95357 : 2025-08-08 01:00:11.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95370 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98172 #locale: "en_US" #translatable: App\Entity\Product\Product {#95363} #id: 36253 #name: "IEEE 1431-2004/Cor 1:2008 (R2010)" #slug: "ieee-1431-2004-cor-1-2008-r2010-ieee00004143-241963" #description: """ Corrigendum Standard - Inactive-Reserved.<br />\n Corrigendum to IEEE Std 1431-2004.<br />\n \t\t\t\t<br />\n Correction of labeling errors on several figures.<br />\n Establish consistent use of symbols and terminology. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros - Corrigendum 1" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95372 …} #channels: Doctrine\ORM\PersistentCollection {#95378 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95374 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95376 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95364 …} -apiLastModifiedAt: DateTime @1754517600 {#95358 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1618524000 {#95359 : 2021-04-16 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1223503200 {#95360 : 2008-10-09 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: DateTime @1269471600 {#95361 : 2010-03-25 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1616626800 {#95362 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "1431" -bookCollection: "" -pageCount: 79 -documents: Doctrine\ORM\PersistentCollection {#95366 …} -favorites: Doctrine\ORM\PersistentCollection {#95368 …} } ] |
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| Attributes | [ "showFullLabel" => false ] |
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| ProductMostRecent | App\Twig\Components\ProductMostRecent | 82.0 MiB | 0.61 ms | |
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| ProductCard | App\Twig\Components\ProductCard | 82.0 MiB | 6.05 ms | |
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| ProductState | App\Twig\Components\ProductState | 82.0 MiB | 0.18 ms | |
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| Attributes | [ "showFullLabel" => false ] |
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| ProductMostRecent | App\Twig\Components\ProductMostRecent | 82.0 MiB | 0.60 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95393 #id: 11188 #code: "IEEE00005700" #attributes: Doctrine\ORM\PersistentCollection {#95410 …} #variants: Doctrine\ORM\PersistentCollection {#95412 …} #options: Doctrine\ORM\PersistentCollection {#95416 …} #associations: Doctrine\ORM\PersistentCollection {#95414 …} #createdAt: DateTime @1751039535 {#95388 : 2025-06-27 17:52:15.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1753969918 {#95389 : 2025-07-31 15:51:58.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95400 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98389 #locale: "en_US" #translatable: App\Entity\Product\Product {#95393} #id: 39761 #name: "IEEE 1780:2022" #slug: "ieee-1780-2022-ieee00005700-242840" #description: """ New IEEE Standard - Active.<br />\n Preparation of an inertial measurement unit (IMU) specification document is discussed in this standard. An outline is provided along with guidance for tailoring.<br />\n \t\t\t\t<br />\n This standard provides an outline of an inertial measurement unit (IMU) specification document and guidance for tailoring the specification.<br />\n This standard provides the specifications, typical units, format, and terminology to specify IMUs. This standard allows users to select which specifications are relevant to their particular applications. The terminology is that which is commonly used by the inertial navigation community. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard for Specifying Inertial Measurement Units (IMUs)" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95402 …} #channels: Doctrine\ORM\PersistentCollection {#95408 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95404 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95406 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95394 …} -apiLastModifiedAt: DateTime @1743289200 {#95390 : 2025-03-30 00:00:00.0 Europe/Paris (+01:00) } -lastUpdatedAt: DateTime @1653256800 {#95391 : 2022-05-23 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1650578400 {#95392 : 2022-04-22 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: null -edition: null -coreDocument: "1780" -bookCollection: "" -pageCount: 61 -documents: Doctrine\ORM\PersistentCollection {#95396 …} -favorites: Doctrine\ORM\PersistentCollection {#95398 …} } ] |
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| Attributes | [] |
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| ProductCard | App\Twig\Components\ProductCard | 82.0 MiB | 6.07 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95424 #id: 11216 #code: "IEEE00005750" #attributes: Doctrine\ORM\PersistentCollection {#95441 …} #variants: Doctrine\ORM\PersistentCollection {#95443 …} #options: Doctrine\ORM\PersistentCollection {#95447 …} #associations: Doctrine\ORM\PersistentCollection {#95445 …} #createdAt: DateTime @1751039553 {#95418 : 2025-06-27 17:52:33.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1753969918 {#95419 : 2025-07-31 15:51:58.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95431 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98619 #locale: "en_US" #translatable: App\Entity\Product\Product {#95424} #id: 39873 #name: "IEEE 293-1969/Cor 1:2014" #slug: "ieee-293-1969-cor-1-2014-ieee00005750-242868" #description: """ Corrigendum Standard - Inactive-Reserved.<br />\n Correction to Table 1 on page 14 of IEEE Std 293-1969<br />\n \t\t\t\t<br />\n This Test Procedure is a compilation of recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered. In some cases alternate methods for measuring a performance characteristic have been included. In selecting among the alternates, attention should be paid to the intended application of the gyro, available test facilities, and the standard methods in use by the test facility. This docu\u{AD}ment is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Standards Publication No.292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros. The intent is for the specification writer to extract the applicable test conditions and equipment from Section 3 of this document for inclusion in the paragraphs concerning test conditions and equipment corresponding to paragraph 4.5 of the Specification Format. Similarly, it is intended that the writer extract the applicable test procedures from Section 4 of this Procedure for inclusion in the paragraphs concerning test procedures, corresponding to the paragraphs listed under paragraph 4.6 of the Specification Format. This Test Procedure can also be used as a guide in the prep\u{AD}aration of a rate gyro test specification, but would require reorganization into the proper Specification Format.<br />\n Blanks have been used in this document for two distinct purposes. One purpose is to provide for<br />\n selection of specific values of test parameters and their tolerances. Other blanks are to be filled<br />\n in with the number of the applicable paragraph from Requirements Section 3 of the specifi\u{AD} cation<br />\n being written.<br />\n Aerospace Industries Association EETC Report No. 5 (Revision A), "Standard Gyro Terminology"* has<br />\n been utilized in the preparation of this Test Procedure. Al\u{AD} though this Procedure is limited to<br />\n electrically energized single-degree-of-freedom spring-restrained rate gyros, it can be<br />\n used as a guide in the preparation of Test Pro\u{AD}Procedures<br />\n for other types of rate gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard for IEEE Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros -- Corrigendum 1: Table 1 Heading" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95433 …} #channels: Doctrine\ORM\PersistentCollection {#95439 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95435 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95437 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95425 …} -apiLastModifiedAt: DateTime @1743289200 {#95420 : 2025-03-30 00:00:00.0 Europe/Paris (+01:00) } -lastUpdatedAt: DateTime @1618178400 {#95421 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1417734000 {#95422 : 2014-12-05 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1616626800 {#95423 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "293" -bookCollection: "" -pageCount: 14 -documents: Doctrine\ORM\PersistentCollection {#95427 …} -favorites: Doctrine\ORM\PersistentCollection {#95429 …} } "layout" => "vertical" "showPrice" => true "showStatusBadges" => true "imageFilter" => "product_listing_thumbnail" "additionalClasses" => "h-100 border-0" "hasStretchedLink" => true "backgroundColor" => "secondary-lighter" "hoverType" => "border-black" ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductCard {#98599 +product: App\Entity\Product\Product {#95424 #id: 11216 #code: "IEEE00005750" #attributes: Doctrine\ORM\PersistentCollection {#95441 …} #variants: Doctrine\ORM\PersistentCollection {#95443 …} #options: Doctrine\ORM\PersistentCollection {#95447 …} #associations: Doctrine\ORM\PersistentCollection {#95445 …} #createdAt: DateTime @1751039553 {#95418 : 2025-06-27 17:52:33.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1753969918 {#95419 : 2025-07-31 15:51:58.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95431 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98619 #locale: "en_US" #translatable: App\Entity\Product\Product {#95424} #id: 39873 #name: "IEEE 293-1969/Cor 1:2014" #slug: "ieee-293-1969-cor-1-2014-ieee00005750-242868" #description: """ Corrigendum Standard - Inactive-Reserved.<br />\n Correction to Table 1 on page 14 of IEEE Std 293-1969<br />\n \t\t\t\t<br />\n This Test Procedure is a compilation of recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered. In some cases alternate methods for measuring a performance characteristic have been included. In selecting among the alternates, attention should be paid to the intended application of the gyro, available test facilities, and the standard methods in use by the test facility. This docu\u{AD}ment is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Standards Publication No.292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros. The intent is for the specification writer to extract the applicable test conditions and equipment from Section 3 of this document for inclusion in the paragraphs concerning test conditions and equipment corresponding to paragraph 4.5 of the Specification Format. Similarly, it is intended that the writer extract the applicable test procedures from Section 4 of this Procedure for inclusion in the paragraphs concerning test procedures, corresponding to the paragraphs listed under paragraph 4.6 of the Specification Format. This Test Procedure can also be used as a guide in the prep\u{AD}aration of a rate gyro test specification, but would require reorganization into the proper Specification Format.<br />\n Blanks have been used in this document for two distinct purposes. One purpose is to provide for<br />\n selection of specific values of test parameters and their tolerances. Other blanks are to be filled<br />\n in with the number of the applicable paragraph from Requirements Section 3 of the specifi\u{AD} cation<br />\n being written.<br />\n Aerospace Industries Association EETC Report No. 5 (Revision A), "Standard Gyro Terminology"* has<br />\n been utilized in the preparation of this Test Procedure. Al\u{AD} though this Procedure is limited to<br />\n electrically energized single-degree-of-freedom spring-restrained rate gyros, it can be<br />\n used as a guide in the preparation of Test Pro\u{AD}Procedures<br />\n for other types of rate gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard for IEEE Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros -- Corrigendum 1: Table 1 Heading" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95433 …} #channels: Doctrine\ORM\PersistentCollection {#95439 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95435 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95437 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95425 …} -apiLastModifiedAt: DateTime @1743289200 {#95420 : 2025-03-30 00:00:00.0 Europe/Paris (+01:00) } -lastUpdatedAt: DateTime @1618178400 {#95421 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1417734000 {#95422 : 2014-12-05 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1616626800 {#95423 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "293" -bookCollection: "" -pageCount: 14 -documents: Doctrine\ORM\PersistentCollection {#95427 …} -favorites: Doctrine\ORM\PersistentCollection {#95429 …} } +layout: "vertical" +showPrice: true +showStatusBadges: true +additionalClasses: "h-100 border-0" +linkLabel: "" +imageFilter: "product_listing_thumbnail" +hasStretchedLink: true +backgroundColor: "secondary-lighter" +hoverType: "border-black" } |
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| ProductState | App\Twig\Components\ProductState | 82.0 MiB | 0.19 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95424 #id: 11216 #code: "IEEE00005750" #attributes: Doctrine\ORM\PersistentCollection {#95441 …} #variants: Doctrine\ORM\PersistentCollection {#95443 …} #options: Doctrine\ORM\PersistentCollection {#95447 …} #associations: Doctrine\ORM\PersistentCollection {#95445 …} #createdAt: DateTime @1751039553 {#95418 : 2025-06-27 17:52:33.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1753969918 {#95419 : 2025-07-31 15:51:58.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95431 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98619 #locale: "en_US" #translatable: App\Entity\Product\Product {#95424} #id: 39873 #name: "IEEE 293-1969/Cor 1:2014" #slug: "ieee-293-1969-cor-1-2014-ieee00005750-242868" #description: """ Corrigendum Standard - Inactive-Reserved.<br />\n Correction to Table 1 on page 14 of IEEE Std 293-1969<br />\n \t\t\t\t<br />\n This Test Procedure is a compilation of recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered. In some cases alternate methods for measuring a performance characteristic have been included. In selecting among the alternates, attention should be paid to the intended application of the gyro, available test facilities, and the standard methods in use by the test facility. This docu\u{AD}ment is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Standards Publication No.292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros. The intent is for the specification writer to extract the applicable test conditions and equipment from Section 3 of this document for inclusion in the paragraphs concerning test conditions and equipment corresponding to paragraph 4.5 of the Specification Format. Similarly, it is intended that the writer extract the applicable test procedures from Section 4 of this Procedure for inclusion in the paragraphs concerning test procedures, corresponding to the paragraphs listed under paragraph 4.6 of the Specification Format. This Test Procedure can also be used as a guide in the prep\u{AD}aration of a rate gyro test specification, but would require reorganization into the proper Specification Format.<br />\n Blanks have been used in this document for two distinct purposes. One purpose is to provide for<br />\n selection of specific values of test parameters and their tolerances. Other blanks are to be filled<br />\n in with the number of the applicable paragraph from Requirements Section 3 of the specifi\u{AD} cation<br />\n being written.<br />\n Aerospace Industries Association EETC Report No. 5 (Revision A), "Standard Gyro Terminology"* has<br />\n been utilized in the preparation of this Test Procedure. Al\u{AD} though this Procedure is limited to<br />\n electrically energized single-degree-of-freedom spring-restrained rate gyros, it can be<br />\n used as a guide in the preparation of Test Pro\u{AD}Procedures<br />\n for other types of rate gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard for IEEE Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros -- Corrigendum 1: Table 1 Heading" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95433 …} #channels: Doctrine\ORM\PersistentCollection {#95439 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95435 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95437 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95425 …} -apiLastModifiedAt: DateTime @1743289200 {#95420 : 2025-03-30 00:00:00.0 Europe/Paris (+01:00) } -lastUpdatedAt: DateTime @1618178400 {#95421 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1417734000 {#95422 : 2014-12-05 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1616626800 {#95423 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "293" -bookCollection: "" -pageCount: 14 -documents: Doctrine\ORM\PersistentCollection {#95427 …} -favorites: Doctrine\ORM\PersistentCollection {#95429 …} } ] |
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| Attributes | [ "showFullLabel" => false ] |
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| Component | App\Twig\Components\ProductState {#98626 +product: App\Entity\Product\Product {#95424 #id: 11216 #code: "IEEE00005750" #attributes: Doctrine\ORM\PersistentCollection {#95441 …} #variants: Doctrine\ORM\PersistentCollection {#95443 …} #options: Doctrine\ORM\PersistentCollection {#95447 …} #associations: Doctrine\ORM\PersistentCollection {#95445 …} #createdAt: DateTime @1751039553 {#95418 : 2025-06-27 17:52:33.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1753969918 {#95419 : 2025-07-31 15:51:58.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95431 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98619 #locale: "en_US" #translatable: App\Entity\Product\Product {#95424} #id: 39873 #name: "IEEE 293-1969/Cor 1:2014" #slug: "ieee-293-1969-cor-1-2014-ieee00005750-242868" #description: """ Corrigendum Standard - Inactive-Reserved.<br />\n Correction to Table 1 on page 14 of IEEE Std 293-1969<br />\n \t\t\t\t<br />\n This Test Procedure is a compilation of recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered. In some cases alternate methods for measuring a performance characteristic have been included. In selecting among the alternates, attention should be paid to the intended application of the gyro, available test facilities, and the standard methods in use by the test facility. This docu\u{AD}ment is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Standards Publication No.292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros. The intent is for the specification writer to extract the applicable test conditions and equipment from Section 3 of this document for inclusion in the paragraphs concerning test conditions and equipment corresponding to paragraph 4.5 of the Specification Format. Similarly, it is intended that the writer extract the applicable test procedures from Section 4 of this Procedure for inclusion in the paragraphs concerning test procedures, corresponding to the paragraphs listed under paragraph 4.6 of the Specification Format. This Test Procedure can also be used as a guide in the prep\u{AD}aration of a rate gyro test specification, but would require reorganization into the proper Specification Format.<br />\n Blanks have been used in this document for two distinct purposes. One purpose is to provide for<br />\n selection of specific values of test parameters and their tolerances. Other blanks are to be filled<br />\n in with the number of the applicable paragraph from Requirements Section 3 of the specifi\u{AD} cation<br />\n being written.<br />\n Aerospace Industries Association EETC Report No. 5 (Revision A), "Standard Gyro Terminology"* has<br />\n been utilized in the preparation of this Test Procedure. Al\u{AD} though this Procedure is limited to<br />\n electrically energized single-degree-of-freedom spring-restrained rate gyros, it can be<br />\n used as a guide in the preparation of Test Pro\u{AD}Procedures<br />\n for other types of rate gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard for IEEE Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros -- Corrigendum 1: Table 1 Heading" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95433 …} #channels: Doctrine\ORM\PersistentCollection {#95439 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95435 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95437 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95425 …} -apiLastModifiedAt: DateTime @1743289200 {#95420 : 2025-03-30 00:00:00.0 Europe/Paris (+01:00) } -lastUpdatedAt: DateTime @1618178400 {#95421 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1417734000 {#95422 : 2014-12-05 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1616626800 {#95423 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "293" -bookCollection: "" -pageCount: 14 -documents: Doctrine\ORM\PersistentCollection {#95427 …} -favorites: Doctrine\ORM\PersistentCollection {#95429 …} } +appearance: "state-withdrawn" +labels: [ "Withdrawn" ] -stateAttributeCode: "state" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductMostRecent | App\Twig\Components\ProductMostRecent | 82.0 MiB | 0.69 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95424 #id: 11216 #code: "IEEE00005750" #attributes: Doctrine\ORM\PersistentCollection {#95441 …} #variants: Doctrine\ORM\PersistentCollection {#95443 …} #options: Doctrine\ORM\PersistentCollection {#95447 …} #associations: Doctrine\ORM\PersistentCollection {#95445 …} #createdAt: DateTime @1751039553 {#95418 : 2025-06-27 17:52:33.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1753969918 {#95419 : 2025-07-31 15:51:58.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95431 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98619 #locale: "en_US" #translatable: App\Entity\Product\Product {#95424} #id: 39873 #name: "IEEE 293-1969/Cor 1:2014" #slug: "ieee-293-1969-cor-1-2014-ieee00005750-242868" #description: """ Corrigendum Standard - Inactive-Reserved.<br />\n Correction to Table 1 on page 14 of IEEE Std 293-1969<br />\n \t\t\t\t<br />\n This Test Procedure is a compilation of recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered. In some cases alternate methods for measuring a performance characteristic have been included. In selecting among the alternates, attention should be paid to the intended application of the gyro, available test facilities, and the standard methods in use by the test facility. This docu\u{AD}ment is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Standards Publication No.292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros. The intent is for the specification writer to extract the applicable test conditions and equipment from Section 3 of this document for inclusion in the paragraphs concerning test conditions and equipment corresponding to paragraph 4.5 of the Specification Format. Similarly, it is intended that the writer extract the applicable test procedures from Section 4 of this Procedure for inclusion in the paragraphs concerning test procedures, corresponding to the paragraphs listed under paragraph 4.6 of the Specification Format. This Test Procedure can also be used as a guide in the prep\u{AD}aration of a rate gyro test specification, but would require reorganization into the proper Specification Format.<br />\n Blanks have been used in this document for two distinct purposes. One purpose is to provide for<br />\n selection of specific values of test parameters and their tolerances. Other blanks are to be filled<br />\n in with the number of the applicable paragraph from Requirements Section 3 of the specifi\u{AD} cation<br />\n being written.<br />\n Aerospace Industries Association EETC Report No. 5 (Revision A), "Standard Gyro Terminology"* has<br />\n been utilized in the preparation of this Test Procedure. Al\u{AD} though this Procedure is limited to<br />\n electrically energized single-degree-of-freedom spring-restrained rate gyros, it can be<br />\n used as a guide in the preparation of Test Pro\u{AD}Procedures<br />\n for other types of rate gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard for IEEE Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros -- Corrigendum 1: Table 1 Heading" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95433 …} #channels: Doctrine\ORM\PersistentCollection {#95439 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95435 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95437 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95425 …} -apiLastModifiedAt: DateTime @1743289200 {#95420 : 2025-03-30 00:00:00.0 Europe/Paris (+01:00) } -lastUpdatedAt: DateTime @1618178400 {#95421 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1417734000 {#95422 : 2014-12-05 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1616626800 {#95423 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "293" -bookCollection: "" -pageCount: 14 -documents: Doctrine\ORM\PersistentCollection {#95427 …} -favorites: Doctrine\ORM\PersistentCollection {#95429 …} } ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductMostRecent {#98703 +product: App\Entity\Product\Product {#95424 #id: 11216 #code: "IEEE00005750" #attributes: Doctrine\ORM\PersistentCollection {#95441 …} #variants: Doctrine\ORM\PersistentCollection {#95443 …} #options: Doctrine\ORM\PersistentCollection {#95447 …} #associations: Doctrine\ORM\PersistentCollection {#95445 …} #createdAt: DateTime @1751039553 {#95418 : 2025-06-27 17:52:33.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1753969918 {#95419 : 2025-07-31 15:51:58.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95431 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98619 #locale: "en_US" #translatable: App\Entity\Product\Product {#95424} #id: 39873 #name: "IEEE 293-1969/Cor 1:2014" #slug: "ieee-293-1969-cor-1-2014-ieee00005750-242868" #description: """ Corrigendum Standard - Inactive-Reserved.<br />\n Correction to Table 1 on page 14 of IEEE Std 293-1969<br />\n \t\t\t\t<br />\n This Test Procedure is a compilation of recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered. In some cases alternate methods for measuring a performance characteristic have been included. In selecting among the alternates, attention should be paid to the intended application of the gyro, available test facilities, and the standard methods in use by the test facility. This docu\u{AD}ment is intended to be a guide in the preparation of Section 4 of a specification that follows the format of IEEE Standards Publication No.292, Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros. The intent is for the specification writer to extract the applicable test conditions and equipment from Section 3 of this document for inclusion in the paragraphs concerning test conditions and equipment corresponding to paragraph 4.5 of the Specification Format. Similarly, it is intended that the writer extract the applicable test procedures from Section 4 of this Procedure for inclusion in the paragraphs concerning test procedures, corresponding to the paragraphs listed under paragraph 4.6 of the Specification Format. This Test Procedure can also be used as a guide in the prep\u{AD}aration of a rate gyro test specification, but would require reorganization into the proper Specification Format.<br />\n Blanks have been used in this document for two distinct purposes. One purpose is to provide for<br />\n selection of specific values of test parameters and their tolerances. Other blanks are to be filled<br />\n in with the number of the applicable paragraph from Requirements Section 3 of the specifi\u{AD} cation<br />\n being written.<br />\n Aerospace Industries Association EETC Report No. 5 (Revision A), "Standard Gyro Terminology"* has<br />\n been utilized in the preparation of this Test Procedure. Al\u{AD} though this Procedure is limited to<br />\n electrically energized single-degree-of-freedom spring-restrained rate gyros, it can be<br />\n used as a guide in the preparation of Test Pro\u{AD}Procedures<br />\n for other types of rate gyros. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard for IEEE Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros -- Corrigendum 1: Table 1 Heading" -notes: "Inactive-Reserved" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95433 …} #channels: Doctrine\ORM\PersistentCollection {#95439 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95435 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95437 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95425 …} -apiLastModifiedAt: DateTime @1743289200 {#95420 : 2025-03-30 00:00:00.0 Europe/Paris (+01:00) } -lastUpdatedAt: DateTime @1618178400 {#95421 : 2021-04-12 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @1417734000 {#95422 : 2014-12-05 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @1616626800 {#95423 : 2021-03-25 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "293" -bookCollection: "" -pageCount: 14 -documents: Doctrine\ORM\PersistentCollection {#95427 …} -favorites: Doctrine\ORM\PersistentCollection {#95429 …} } +label: "Most Recent" +icon: "check-xs" -mostRecentAttributeCode: "most_recent" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductCard | App\Twig\Components\ProductCard | 82.0 MiB | 5.52 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95454 #id: 11233 #code: "IEEE00005780" #attributes: Doctrine\ORM\PersistentCollection {#95471 …} #variants: Doctrine\ORM\PersistentCollection {#95473 …} #options: Doctrine\ORM\PersistentCollection {#95477 …} #associations: Doctrine\ORM\PersistentCollection {#95475 …} #createdAt: DateTime @1751039563 {#95449 : 2025-06-27 17:52:43.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754608621 {#95450 : 2025-08-08 01:17:01.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95461 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98828 #locale: "en_US" #translatable: App\Entity\Product\Product {#95454} #id: 39941 #name: "IEEE 529-1980/Cor 1:2017" #slug: "ieee-529-1980-cor-1-2017-ieee00005780-242885" #description: """ Corrigendum Standard - Active.<br />\n Corrections are made by this corrigendum to material already published in IEEE Std 529-1980.<br />\n \t\t\t\t<br />\n This corrigendum will not change any portion of the document that is not covered in the original scope of 529-1980. The scope of the proposed corrigenda includes changes as follows. There are two missing division symbols in the units of clause 3.3.9.2.2 Item 2. Another change is there is an omega in section 6.3 that is superscript but should be subscripted. The equation in clause 10.10.4.1 needs to be corrected because there is a typesetting issue where the equation is on two lines and there is an extraneous X. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros - Corrigendum 1: 3.3.9.2.2, 3.6.4.1.1, 3.6.4.1.2, 6.3, and 10.10.4.1" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95463 …} #channels: Doctrine\ORM\PersistentCollection {#95469 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95465 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95467 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95455 …} -apiLastModifiedAt: DateTime @1754517600 {#95451 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95452 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1508968800 {#95453 : 2017-10-26 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: null -edition: null -coreDocument: "529" -bookCollection: "" -pageCount: 13 -documents: Doctrine\ORM\PersistentCollection {#95457 …} -favorites: Doctrine\ORM\PersistentCollection {#95459 …} } "layout" => "vertical" "showPrice" => true "showStatusBadges" => true "imageFilter" => "product_listing_thumbnail" "additionalClasses" => "h-100 border-0" "hasStretchedLink" => true "backgroundColor" => "white" "hoverType" => "border-black" ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductCard {#98808 +product: App\Entity\Product\Product {#95454 #id: 11233 #code: "IEEE00005780" #attributes: Doctrine\ORM\PersistentCollection {#95471 …} #variants: Doctrine\ORM\PersistentCollection {#95473 …} #options: Doctrine\ORM\PersistentCollection {#95477 …} #associations: Doctrine\ORM\PersistentCollection {#95475 …} #createdAt: DateTime @1751039563 {#95449 : 2025-06-27 17:52:43.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754608621 {#95450 : 2025-08-08 01:17:01.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95461 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98828 #locale: "en_US" #translatable: App\Entity\Product\Product {#95454} #id: 39941 #name: "IEEE 529-1980/Cor 1:2017" #slug: "ieee-529-1980-cor-1-2017-ieee00005780-242885" #description: """ Corrigendum Standard - Active.<br />\n Corrections are made by this corrigendum to material already published in IEEE Std 529-1980.<br />\n \t\t\t\t<br />\n This corrigendum will not change any portion of the document that is not covered in the original scope of 529-1980. The scope of the proposed corrigenda includes changes as follows. There are two missing division symbols in the units of clause 3.3.9.2.2 Item 2. Another change is there is an omega in section 6.3 that is superscript but should be subscripted. The equation in clause 10.10.4.1 needs to be corrected because there is a typesetting issue where the equation is on two lines and there is an extraneous X. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros - Corrigendum 1: 3.3.9.2.2, 3.6.4.1.1, 3.6.4.1.2, 6.3, and 10.10.4.1" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95463 …} #channels: Doctrine\ORM\PersistentCollection {#95469 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95465 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95467 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95455 …} -apiLastModifiedAt: DateTime @1754517600 {#95451 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95452 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1508968800 {#95453 : 2017-10-26 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: null -edition: null -coreDocument: "529" -bookCollection: "" -pageCount: 13 -documents: Doctrine\ORM\PersistentCollection {#95457 …} -favorites: Doctrine\ORM\PersistentCollection {#95459 …} } +layout: "vertical" +showPrice: true +showStatusBadges: true +additionalClasses: "h-100 border-0" +linkLabel: "" +imageFilter: "product_listing_thumbnail" +hasStretchedLink: true +backgroundColor: "white" +hoverType: "border-black" } |
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| ProductState | App\Twig\Components\ProductState | 82.0 MiB | 0.17 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95454 #id: 11233 #code: "IEEE00005780" #attributes: Doctrine\ORM\PersistentCollection {#95471 …} #variants: Doctrine\ORM\PersistentCollection {#95473 …} #options: Doctrine\ORM\PersistentCollection {#95477 …} #associations: Doctrine\ORM\PersistentCollection {#95475 …} #createdAt: DateTime @1751039563 {#95449 : 2025-06-27 17:52:43.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754608621 {#95450 : 2025-08-08 01:17:01.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95461 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98828 #locale: "en_US" #translatable: App\Entity\Product\Product {#95454} #id: 39941 #name: "IEEE 529-1980/Cor 1:2017" #slug: "ieee-529-1980-cor-1-2017-ieee00005780-242885" #description: """ Corrigendum Standard - Active.<br />\n Corrections are made by this corrigendum to material already published in IEEE Std 529-1980.<br />\n \t\t\t\t<br />\n This corrigendum will not change any portion of the document that is not covered in the original scope of 529-1980. The scope of the proposed corrigenda includes changes as follows. There are two missing division symbols in the units of clause 3.3.9.2.2 Item 2. Another change is there is an omega in section 6.3 that is superscript but should be subscripted. The equation in clause 10.10.4.1 needs to be corrected because there is a typesetting issue where the equation is on two lines and there is an extraneous X. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros - Corrigendum 1: 3.3.9.2.2, 3.6.4.1.1, 3.6.4.1.2, 6.3, and 10.10.4.1" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95463 …} #channels: Doctrine\ORM\PersistentCollection {#95469 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95465 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95467 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95455 …} -apiLastModifiedAt: DateTime @1754517600 {#95451 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95452 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1508968800 {#95453 : 2017-10-26 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: null -edition: null -coreDocument: "529" -bookCollection: "" -pageCount: 13 -documents: Doctrine\ORM\PersistentCollection {#95457 …} -favorites: Doctrine\ORM\PersistentCollection {#95459 …} } ] |
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| Attributes | [ "showFullLabel" => false ] |
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| Component | App\Twig\Components\ProductState {#98835 +product: App\Entity\Product\Product {#95454 #id: 11233 #code: "IEEE00005780" #attributes: Doctrine\ORM\PersistentCollection {#95471 …} #variants: Doctrine\ORM\PersistentCollection {#95473 …} #options: Doctrine\ORM\PersistentCollection {#95477 …} #associations: Doctrine\ORM\PersistentCollection {#95475 …} #createdAt: DateTime @1751039563 {#95449 : 2025-06-27 17:52:43.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754608621 {#95450 : 2025-08-08 01:17:01.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95461 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98828 #locale: "en_US" #translatable: App\Entity\Product\Product {#95454} #id: 39941 #name: "IEEE 529-1980/Cor 1:2017" #slug: "ieee-529-1980-cor-1-2017-ieee00005780-242885" #description: """ Corrigendum Standard - Active.<br />\n Corrections are made by this corrigendum to material already published in IEEE Std 529-1980.<br />\n \t\t\t\t<br />\n This corrigendum will not change any portion of the document that is not covered in the original scope of 529-1980. The scope of the proposed corrigenda includes changes as follows. There are two missing division symbols in the units of clause 3.3.9.2.2 Item 2. Another change is there is an omega in section 6.3 that is superscript but should be subscripted. The equation in clause 10.10.4.1 needs to be corrected because there is a typesetting issue where the equation is on two lines and there is an extraneous X. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros - Corrigendum 1: 3.3.9.2.2, 3.6.4.1.1, 3.6.4.1.2, 6.3, and 10.10.4.1" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95463 …} #channels: Doctrine\ORM\PersistentCollection {#95469 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95465 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95467 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95455 …} -apiLastModifiedAt: DateTime @1754517600 {#95451 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95452 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1508968800 {#95453 : 2017-10-26 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: null -edition: null -coreDocument: "529" -bookCollection: "" -pageCount: 13 -documents: Doctrine\ORM\PersistentCollection {#95457 …} -favorites: Doctrine\ORM\PersistentCollection {#95459 …} } +appearance: "state-active" +labels: [ "Active" ] -stateAttributeCode: "state" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductMostRecent | App\Twig\Components\ProductMostRecent | 82.0 MiB | 0.58 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#95454 #id: 11233 #code: "IEEE00005780" #attributes: Doctrine\ORM\PersistentCollection {#95471 …} #variants: Doctrine\ORM\PersistentCollection {#95473 …} #options: Doctrine\ORM\PersistentCollection {#95477 …} #associations: Doctrine\ORM\PersistentCollection {#95475 …} #createdAt: DateTime @1751039563 {#95449 : 2025-06-27 17:52:43.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754608621 {#95450 : 2025-08-08 01:17:01.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95461 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98828 #locale: "en_US" #translatable: App\Entity\Product\Product {#95454} #id: 39941 #name: "IEEE 529-1980/Cor 1:2017" #slug: "ieee-529-1980-cor-1-2017-ieee00005780-242885" #description: """ Corrigendum Standard - Active.<br />\n Corrections are made by this corrigendum to material already published in IEEE Std 529-1980.<br />\n \t\t\t\t<br />\n This corrigendum will not change any portion of the document that is not covered in the original scope of 529-1980. The scope of the proposed corrigenda includes changes as follows. There are two missing division symbols in the units of clause 3.3.9.2.2 Item 2. Another change is there is an omega in section 6.3 that is superscript but should be subscripted. The equation in clause 10.10.4.1 needs to be corrected because there is a typesetting issue where the equation is on two lines and there is an extraneous X. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros - Corrigendum 1: 3.3.9.2.2, 3.6.4.1.1, 3.6.4.1.2, 6.3, and 10.10.4.1" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95463 …} #channels: Doctrine\ORM\PersistentCollection {#95469 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95465 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95467 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95455 …} -apiLastModifiedAt: DateTime @1754517600 {#95451 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95452 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1508968800 {#95453 : 2017-10-26 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: null -edition: null -coreDocument: "529" -bookCollection: "" -pageCount: 13 -documents: Doctrine\ORM\PersistentCollection {#95457 …} -favorites: Doctrine\ORM\PersistentCollection {#95459 …} } ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductMostRecent {#98912 +product: App\Entity\Product\Product {#95454 #id: 11233 #code: "IEEE00005780" #attributes: Doctrine\ORM\PersistentCollection {#95471 …} #variants: Doctrine\ORM\PersistentCollection {#95473 …} #options: Doctrine\ORM\PersistentCollection {#95477 …} #associations: Doctrine\ORM\PersistentCollection {#95475 …} #createdAt: DateTime @1751039563 {#95449 : 2025-06-27 17:52:43.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754608621 {#95450 : 2025-08-08 01:17:01.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#95461 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#98828 #locale: "en_US" #translatable: App\Entity\Product\Product {#95454} #id: 39941 #name: "IEEE 529-1980/Cor 1:2017" #slug: "ieee-529-1980-cor-1-2017-ieee00005780-242885" #description: """ Corrigendum Standard - Active.<br />\n Corrections are made by this corrigendum to material already published in IEEE Std 529-1980.<br />\n \t\t\t\t<br />\n This corrigendum will not change any portion of the document that is not covered in the original scope of 529-1980. The scope of the proposed corrigenda includes changes as follows. There are two missing division symbols in the units of clause 3.3.9.2.2 Item 2. Another change is there is an omega in section 6.3 that is superscript but should be subscripted. The equation in clause 10.10.4.1 needs to be corrected because there is a typesetting issue where the equation is on two lines and there is an extraneous X. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros - Corrigendum 1: 3.3.9.2.2, 3.6.4.1.1, 3.6.4.1.2, 6.3, and 10.10.4.1" -notes: "Active" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#95463 …} #channels: Doctrine\ORM\PersistentCollection {#95469 …} #mainTaxon: App\Entity\Taxonomy\Taxon {#8840 …} #reviews: Doctrine\ORM\PersistentCollection {#95465 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#95467 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#95069 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#95455 …} -apiLastModifiedAt: DateTime @1754517600 {#95451 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#95452 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @1508968800 {#95453 : 2017-10-26 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: null -canceledAt: null -edition: null -coreDocument: "529" -bookCollection: "" -pageCount: 13 -documents: Doctrine\ORM\PersistentCollection {#95457 …} -favorites: Doctrine\ORM\PersistentCollection {#95459 …} } +label: "Most Recent" +icon: "check-xs" -mostRecentAttributeCode: "most_recent" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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