Components
4
Twig Components
8
Render Count
10
ms
Render Time
212.0
MiB
Memory Usage
Components
| Name | Metadata | Render Count | Render Time |
|---|---|---|---|
| ProductState |
"App\Twig\Components\ProductState"components/ProductState.html.twig |
3 | 0.76ms |
| ProductMostRecent |
"App\Twig\Components\ProductMostRecent"components/ProductMostRecent.html.twig |
3 | 2.31ms |
| ProductType |
"App\Twig\Components\ProductType"components/ProductType.html.twig |
1 | 0.22ms |
| ProductCard |
"App\Twig\Components\ProductCard"components/ProductCard.html.twig |
1 | 7.91ms |
Render calls
| ProductState | App\Twig\Components\ProductState | 212.0 MiB | 0.31 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#7309 #id: 8874 #code: "IEEE00001200" #attributes: Doctrine\ORM\PersistentCollection {#7702 …} #variants: Doctrine\ORM\PersistentCollection {#7745 …} #options: Doctrine\ORM\PersistentCollection {#7917 …} #associations: Doctrine\ORM\PersistentCollection {#7901 …} #createdAt: DateTime @1751037782 {#7274 : 2025-06-27 17:23:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#7322 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#7923 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#7922 #locale: "en_US" #translatable: App\Entity\Product\Product {#7309} #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 {#7535 …} #channels: Doctrine\ORM\PersistentCollection {#7629 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#7614 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#7646 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#7420 …} -apiLastModifiedAt: DateTime @1754517600 {#7317 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1648764000 {#7292 : 2022-04-01 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @613000800 {#7318 : 1989-06-05 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: DateTime @1323212400 {#7316 : 2011-12-07 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1648076400 {#7315 : 2022-03-24 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "813" -bookCollection: "" -pageCount: 68 -documents: Doctrine\ORM\PersistentCollection {#7466 …} -favorites: Doctrine\ORM\PersistentCollection {#7501 …} } "showFullLabel" => "true" ] |
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| Attributes | [ "showFullLabel" => "true" ] |
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| Component | App\Twig\Components\ProductState {#93056 +product: App\Entity\Product\Product {#7309 #id: 8874 #code: "IEEE00001200" #attributes: Doctrine\ORM\PersistentCollection {#7702 …} #variants: Doctrine\ORM\PersistentCollection {#7745 …} #options: Doctrine\ORM\PersistentCollection {#7917 …} #associations: Doctrine\ORM\PersistentCollection {#7901 …} #createdAt: DateTime @1751037782 {#7274 : 2025-06-27 17:23:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#7322 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#7923 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#7922 #locale: "en_US" #translatable: App\Entity\Product\Product {#7309} #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 {#7535 …} #channels: Doctrine\ORM\PersistentCollection {#7629 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#7614 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#7646 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#7420 …} -apiLastModifiedAt: DateTime @1754517600 {#7317 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1648764000 {#7292 : 2022-04-01 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @613000800 {#7318 : 1989-06-05 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: DateTime @1323212400 {#7316 : 2011-12-07 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1648076400 {#7315 : 2022-03-24 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "813" -bookCollection: "" -pageCount: 68 -documents: Doctrine\ORM\PersistentCollection {#7466 …} -favorites: Doctrine\ORM\PersistentCollection {#7501 …} } +appearance: "state-withdrawn" +labels: [ "Withdrawn" "Confirmed" ] -stateAttributeCode: "state" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductType | App\Twig\Components\ProductType | 212.0 MiB | 0.22 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#7309 #id: 8874 #code: "IEEE00001200" #attributes: Doctrine\ORM\PersistentCollection {#7702 …} #variants: Doctrine\ORM\PersistentCollection {#7745 …} #options: Doctrine\ORM\PersistentCollection {#7917 …} #associations: Doctrine\ORM\PersistentCollection {#7901 …} #createdAt: DateTime @1751037782 {#7274 : 2025-06-27 17:23:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#7322 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#7923 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#7922 #locale: "en_US" #translatable: App\Entity\Product\Product {#7309} #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 {#7535 …} #channels: Doctrine\ORM\PersistentCollection {#7629 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#7614 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#7646 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#7420 …} -apiLastModifiedAt: DateTime @1754517600 {#7317 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1648764000 {#7292 : 2022-04-01 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @613000800 {#7318 : 1989-06-05 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: DateTime @1323212400 {#7316 : 2011-12-07 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1648076400 {#7315 : 2022-03-24 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "813" -bookCollection: "" -pageCount: 68 -documents: Doctrine\ORM\PersistentCollection {#7466 …} -favorites: Doctrine\ORM\PersistentCollection {#7501 …} } ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductType {#93247 +product: App\Entity\Product\Product {#7309 #id: 8874 #code: "IEEE00001200" #attributes: Doctrine\ORM\PersistentCollection {#7702 …} #variants: Doctrine\ORM\PersistentCollection {#7745 …} #options: Doctrine\ORM\PersistentCollection {#7917 …} #associations: Doctrine\ORM\PersistentCollection {#7901 …} #createdAt: DateTime @1751037782 {#7274 : 2025-06-27 17:23:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#7322 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#7923 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#7922 #locale: "en_US" #translatable: App\Entity\Product\Product {#7309} #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 {#7535 …} #channels: Doctrine\ORM\PersistentCollection {#7629 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#7614 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#7646 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#7420 …} -apiLastModifiedAt: DateTime @1754517600 {#7317 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1648764000 {#7292 : 2022-04-01 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @613000800 {#7318 : 1989-06-05 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: DateTime @1323212400 {#7316 : 2011-12-07 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1648076400 {#7315 : 2022-03-24 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "813" -bookCollection: "" -pageCount: 68 -documents: Doctrine\ORM\PersistentCollection {#7466 …} -favorites: Doctrine\ORM\PersistentCollection {#7501 …} } +label: "Standard" -typeAttributeCode: "type" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductMostRecent | App\Twig\Components\ProductMostRecent | 212.0 MiB | 0.66 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#7309 #id: 8874 #code: "IEEE00001200" #attributes: Doctrine\ORM\PersistentCollection {#7702 …} #variants: Doctrine\ORM\PersistentCollection {#7745 …} #options: Doctrine\ORM\PersistentCollection {#7917 …} #associations: Doctrine\ORM\PersistentCollection {#7901 …} #createdAt: DateTime @1751037782 {#7274 : 2025-06-27 17:23:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#7322 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#7923 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#7922 #locale: "en_US" #translatable: App\Entity\Product\Product {#7309} #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 {#7535 …} #channels: Doctrine\ORM\PersistentCollection {#7629 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#7614 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#7646 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#7420 …} -apiLastModifiedAt: DateTime @1754517600 {#7317 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1648764000 {#7292 : 2022-04-01 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @613000800 {#7318 : 1989-06-05 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: DateTime @1323212400 {#7316 : 2011-12-07 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1648076400 {#7315 : 2022-03-24 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "813" -bookCollection: "" -pageCount: 68 -documents: Doctrine\ORM\PersistentCollection {#7466 …} -favorites: Doctrine\ORM\PersistentCollection {#7501 …} } ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductMostRecent {#93314 +product: App\Entity\Product\Product {#7309 #id: 8874 #code: "IEEE00001200" #attributes: Doctrine\ORM\PersistentCollection {#7702 …} #variants: Doctrine\ORM\PersistentCollection {#7745 …} #options: Doctrine\ORM\PersistentCollection {#7917 …} #associations: Doctrine\ORM\PersistentCollection {#7901 …} #createdAt: DateTime @1751037782 {#7274 : 2025-06-27 17:23:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#7322 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#7923 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#7922 #locale: "en_US" #translatable: App\Entity\Product\Product {#7309} #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 {#7535 …} #channels: Doctrine\ORM\PersistentCollection {#7629 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#7614 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#7646 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#7420 …} -apiLastModifiedAt: DateTime @1754517600 {#7317 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1648764000 {#7292 : 2022-04-01 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @613000800 {#7318 : 1989-06-05 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: DateTime @1323212400 {#7316 : 2011-12-07 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1648076400 {#7315 : 2022-03-24 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "813" -bookCollection: "" -pageCount: 68 -documents: Doctrine\ORM\PersistentCollection {#7466 …} -favorites: Doctrine\ORM\PersistentCollection {#7501 …} } +label: "Most Recent" +icon: "check-xs" -mostRecentAttributeCode: "most_recent" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductState | App\Twig\Components\ProductState | 212.0 MiB | 0.20 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#7309 #id: 8874 #code: "IEEE00001200" #attributes: Doctrine\ORM\PersistentCollection {#7702 …} #variants: Doctrine\ORM\PersistentCollection {#7745 …} #options: Doctrine\ORM\PersistentCollection {#7917 …} #associations: Doctrine\ORM\PersistentCollection {#7901 …} #createdAt: DateTime @1751037782 {#7274 : 2025-06-27 17:23:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#7322 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#7923 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#7922 #locale: "en_US" #translatable: App\Entity\Product\Product {#7309} #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 {#7535 …} #channels: Doctrine\ORM\PersistentCollection {#7629 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#7614 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#7646 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#7420 …} -apiLastModifiedAt: DateTime @1754517600 {#7317 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1648764000 {#7292 : 2022-04-01 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @613000800 {#7318 : 1989-06-05 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: DateTime @1323212400 {#7316 : 2011-12-07 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1648076400 {#7315 : 2022-03-24 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "813" -bookCollection: "" -pageCount: 68 -documents: Doctrine\ORM\PersistentCollection {#7466 …} -favorites: Doctrine\ORM\PersistentCollection {#7501 …} } "showFullLabel" => "true" ] |
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| Attributes | [ "showFullLabel" => "true" ] |
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| Component | App\Twig\Components\ProductState {#106783 +product: App\Entity\Product\Product {#7309 #id: 8874 #code: "IEEE00001200" #attributes: Doctrine\ORM\PersistentCollection {#7702 …} #variants: Doctrine\ORM\PersistentCollection {#7745 …} #options: Doctrine\ORM\PersistentCollection {#7917 …} #associations: Doctrine\ORM\PersistentCollection {#7901 …} #createdAt: DateTime @1751037782 {#7274 : 2025-06-27 17:23:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#7322 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#7923 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#7922 #locale: "en_US" #translatable: App\Entity\Product\Product {#7309} #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 {#7535 …} #channels: Doctrine\ORM\PersistentCollection {#7629 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#7614 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#7646 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#7420 …} -apiLastModifiedAt: DateTime @1754517600 {#7317 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1648764000 {#7292 : 2022-04-01 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @613000800 {#7318 : 1989-06-05 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: DateTime @1323212400 {#7316 : 2011-12-07 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1648076400 {#7315 : 2022-03-24 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "813" -bookCollection: "" -pageCount: 68 -documents: Doctrine\ORM\PersistentCollection {#7466 …} -favorites: Doctrine\ORM\PersistentCollection {#7501 …} } +appearance: "state-withdrawn" +labels: [ "Withdrawn" "Confirmed" ] -stateAttributeCode: "state" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductMostRecent | App\Twig\Components\ProductMostRecent | 212.0 MiB | 0.71 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#7309 #id: 8874 #code: "IEEE00001200" #attributes: Doctrine\ORM\PersistentCollection {#7702 …} #variants: Doctrine\ORM\PersistentCollection {#7745 …} #options: Doctrine\ORM\PersistentCollection {#7917 …} #associations: Doctrine\ORM\PersistentCollection {#7901 …} #createdAt: DateTime @1751037782 {#7274 : 2025-06-27 17:23:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#7322 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#7923 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#7922 #locale: "en_US" #translatable: App\Entity\Product\Product {#7309} #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 {#7535 …} #channels: Doctrine\ORM\PersistentCollection {#7629 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#7614 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#7646 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#7420 …} -apiLastModifiedAt: DateTime @1754517600 {#7317 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1648764000 {#7292 : 2022-04-01 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @613000800 {#7318 : 1989-06-05 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: DateTime @1323212400 {#7316 : 2011-12-07 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1648076400 {#7315 : 2022-03-24 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "813" -bookCollection: "" -pageCount: 68 -documents: Doctrine\ORM\PersistentCollection {#7466 …} -favorites: Doctrine\ORM\PersistentCollection {#7501 …} } ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductMostRecent {#106867 +product: App\Entity\Product\Product {#7309 #id: 8874 #code: "IEEE00001200" #attributes: Doctrine\ORM\PersistentCollection {#7702 …} #variants: Doctrine\ORM\PersistentCollection {#7745 …} #options: Doctrine\ORM\PersistentCollection {#7917 …} #associations: Doctrine\ORM\PersistentCollection {#7901 …} #createdAt: DateTime @1751037782 {#7274 : 2025-06-27 17:23:02.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#7322 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#7923 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#7922 #locale: "en_US" #translatable: App\Entity\Product\Product {#7309} #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 {#7535 …} #channels: Doctrine\ORM\PersistentCollection {#7629 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#7614 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#7646 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#7420 …} -apiLastModifiedAt: DateTime @1754517600 {#7317 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1648764000 {#7292 : 2022-04-01 00:00:00.0 Europe/Paris (+02:00) } -author: "" -publishedAt: DateTime @613000800 {#7318 : 1989-06-05 00:00:00.0 Europe/Paris (+02:00) } -releasedAt: null -confirmedAt: DateTime @1323212400 {#7316 : 2011-12-07 00:00:00.0 Europe/Paris (+01:00) } -canceledAt: DateTime @1648076400 {#7315 : 2022-03-24 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "813" -bookCollection: "" -pageCount: 68 -documents: Doctrine\ORM\PersistentCollection {#7466 …} -favorites: Doctrine\ORM\PersistentCollection {#7501 …} } +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 | 212.0 MiB | 7.91 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#128312 #id: 8635 #code: "IEEE00000778" #attributes: Doctrine\ORM\PersistentCollection {#128295 …} #variants: Doctrine\ORM\PersistentCollection {#128293 …} #options: Doctrine\ORM\PersistentCollection {#128288 …} #associations: Doctrine\ORM\PersistentCollection {#128290 …} #createdAt: DateTime @1751037581 {#128285 : 2025-06-27 17:19:41.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#128319 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#128306 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#128406 #locale: "en_US" #translatable: App\Entity\Product\Product {#128312} #id: 29549 #name: "IEEE 528:1984" #slug: "ieee-528-1984-ieee00000778-240287" #description: """ New IEEE Standard - Inactive-Withdrawn.<br />\n Withdrawn Status. Terms and definitions relating to inertial sensors are presented. Usage as understood by the inertial sensor 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 sensor technology.<br />\n \t\t\t\t<br />\n Terms and definitions relating to inertial sensors are presented. Usage as understood by the inertial sensor 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 sensor technology. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Inertial Sensor Terminology" -notes: "Inactive-Withdrawn" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#128304 …} #channels: Doctrine\ORM\PersistentCollection {#128297 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#128301 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#128299 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#128270 …} -apiLastModifiedAt: DateTime @1754517600 {#128271 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#128313 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @442710000 {#128320 : 1984-01-12 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @691887600 {#128278 : 1991-12-05 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "528" -bookCollection: "" -pageCount: 16 -documents: Doctrine\ORM\PersistentCollection {#128310 …} -favorites: Doctrine\ORM\PersistentCollection {#128308 …} } "layout" => "vertical" "showPrice" => true "showStatusBadges" => true "additionalClasses" => "product__teaser--with-grey-border" "hasStretchedLink" => true "hoverType" => "shadow" "linkLabel" => "See more" ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductCard {#128368 +product: App\Entity\Product\Product {#128312 #id: 8635 #code: "IEEE00000778" #attributes: Doctrine\ORM\PersistentCollection {#128295 …} #variants: Doctrine\ORM\PersistentCollection {#128293 …} #options: Doctrine\ORM\PersistentCollection {#128288 …} #associations: Doctrine\ORM\PersistentCollection {#128290 …} #createdAt: DateTime @1751037581 {#128285 : 2025-06-27 17:19:41.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#128319 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#128306 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#128406 #locale: "en_US" #translatable: App\Entity\Product\Product {#128312} #id: 29549 #name: "IEEE 528:1984" #slug: "ieee-528-1984-ieee00000778-240287" #description: """ New IEEE Standard - Inactive-Withdrawn.<br />\n Withdrawn Status. Terms and definitions relating to inertial sensors are presented. Usage as understood by the inertial sensor 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 sensor technology.<br />\n \t\t\t\t<br />\n Terms and definitions relating to inertial sensors are presented. Usage as understood by the inertial sensor 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 sensor technology. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Inertial Sensor Terminology" -notes: "Inactive-Withdrawn" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#128304 …} #channels: Doctrine\ORM\PersistentCollection {#128297 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#128301 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#128299 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#128270 …} -apiLastModifiedAt: DateTime @1754517600 {#128271 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#128313 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @442710000 {#128320 : 1984-01-12 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @691887600 {#128278 : 1991-12-05 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "528" -bookCollection: "" -pageCount: 16 -documents: Doctrine\ORM\PersistentCollection {#128310 …} -favorites: Doctrine\ORM\PersistentCollection {#128308 …} } +layout: "vertical" +showPrice: true +showStatusBadges: true +additionalClasses: "product__teaser--with-grey-border" +linkLabel: "See more" +imageFilter: "product_thumbnail_teaser" +hasStretchedLink: true +backgroundColor: "white" +hoverType: "shadow" } |
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| ProductState | App\Twig\Components\ProductState | 212.0 MiB | 0.25 ms | |
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| Input props | [ "product" => App\Entity\Product\Product {#128312 #id: 8635 #code: "IEEE00000778" #attributes: Doctrine\ORM\PersistentCollection {#128295 …} #variants: Doctrine\ORM\PersistentCollection {#128293 …} #options: Doctrine\ORM\PersistentCollection {#128288 …} #associations: Doctrine\ORM\PersistentCollection {#128290 …} #createdAt: DateTime @1751037581 {#128285 : 2025-06-27 17:19:41.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#128319 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#128306 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#128406 #locale: "en_US" #translatable: App\Entity\Product\Product {#128312} #id: 29549 #name: "IEEE 528:1984" #slug: "ieee-528-1984-ieee00000778-240287" #description: """ New IEEE Standard - Inactive-Withdrawn.<br />\n Withdrawn Status. Terms and definitions relating to inertial sensors are presented. Usage as understood by the inertial sensor 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 sensor technology.<br />\n \t\t\t\t<br />\n Terms and definitions relating to inertial sensors are presented. Usage as understood by the inertial sensor 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 sensor technology. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Inertial Sensor Terminology" -notes: "Inactive-Withdrawn" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#128304 …} #channels: Doctrine\ORM\PersistentCollection {#128297 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#128301 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#128299 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#128270 …} -apiLastModifiedAt: DateTime @1754517600 {#128271 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#128313 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @442710000 {#128320 : 1984-01-12 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @691887600 {#128278 : 1991-12-05 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "528" -bookCollection: "" -pageCount: 16 -documents: Doctrine\ORM\PersistentCollection {#128310 …} -favorites: Doctrine\ORM\PersistentCollection {#128308 …} } ] |
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| Attributes | [ "showFullLabel" => false ] |
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| Component | App\Twig\Components\ProductState {#128408 +product: App\Entity\Product\Product {#128312 #id: 8635 #code: "IEEE00000778" #attributes: Doctrine\ORM\PersistentCollection {#128295 …} #variants: Doctrine\ORM\PersistentCollection {#128293 …} #options: Doctrine\ORM\PersistentCollection {#128288 …} #associations: Doctrine\ORM\PersistentCollection {#128290 …} #createdAt: DateTime @1751037581 {#128285 : 2025-06-27 17:19:41.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#128319 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#128306 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#128406 #locale: "en_US" #translatable: App\Entity\Product\Product {#128312} #id: 29549 #name: "IEEE 528:1984" #slug: "ieee-528-1984-ieee00000778-240287" #description: """ New IEEE Standard - Inactive-Withdrawn.<br />\n Withdrawn Status. Terms and definitions relating to inertial sensors are presented. Usage as understood by the inertial sensor 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 sensor technology.<br />\n \t\t\t\t<br />\n Terms and definitions relating to inertial sensors are presented. Usage as understood by the inertial sensor 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 sensor technology. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Inertial Sensor Terminology" -notes: "Inactive-Withdrawn" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#128304 …} #channels: Doctrine\ORM\PersistentCollection {#128297 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#128301 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#128299 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#128270 …} -apiLastModifiedAt: DateTime @1754517600 {#128271 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#128313 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @442710000 {#128320 : 1984-01-12 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @691887600 {#128278 : 1991-12-05 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "528" -bookCollection: "" -pageCount: 16 -documents: Doctrine\ORM\PersistentCollection {#128310 …} -favorites: Doctrine\ORM\PersistentCollection {#128308 …} } +appearance: "state-suspended" +labels: [ "Superseded" ] -stateAttributeCode: "state" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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| ProductMostRecent | App\Twig\Components\ProductMostRecent | 212.0 MiB | 0.94 ms | |
|---|---|---|---|---|
| Input props | [ "product" => App\Entity\Product\Product {#128312 #id: 8635 #code: "IEEE00000778" #attributes: Doctrine\ORM\PersistentCollection {#128295 …} #variants: Doctrine\ORM\PersistentCollection {#128293 …} #options: Doctrine\ORM\PersistentCollection {#128288 …} #associations: Doctrine\ORM\PersistentCollection {#128290 …} #createdAt: DateTime @1751037581 {#128285 : 2025-06-27 17:19:41.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#128319 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#128306 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#128406 #locale: "en_US" #translatable: App\Entity\Product\Product {#128312} #id: 29549 #name: "IEEE 528:1984" #slug: "ieee-528-1984-ieee00000778-240287" #description: """ New IEEE Standard - Inactive-Withdrawn.<br />\n Withdrawn Status. Terms and definitions relating to inertial sensors are presented. Usage as understood by the inertial sensor 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 sensor technology.<br />\n \t\t\t\t<br />\n Terms and definitions relating to inertial sensors are presented. Usage as understood by the inertial sensor 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 sensor technology. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Inertial Sensor Terminology" -notes: "Inactive-Withdrawn" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#128304 …} #channels: Doctrine\ORM\PersistentCollection {#128297 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#128301 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#128299 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#128270 …} -apiLastModifiedAt: DateTime @1754517600 {#128271 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#128313 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @442710000 {#128320 : 1984-01-12 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @691887600 {#128278 : 1991-12-05 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "528" -bookCollection: "" -pageCount: 16 -documents: Doctrine\ORM\PersistentCollection {#128310 …} -favorites: Doctrine\ORM\PersistentCollection {#128308 …} } ] |
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| Attributes | [] |
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| Component | App\Twig\Components\ProductMostRecent {#128486 +product: App\Entity\Product\Product {#128312 #id: 8635 #code: "IEEE00000778" #attributes: Doctrine\ORM\PersistentCollection {#128295 …} #variants: Doctrine\ORM\PersistentCollection {#128293 …} #options: Doctrine\ORM\PersistentCollection {#128288 …} #associations: Doctrine\ORM\PersistentCollection {#128290 …} #createdAt: DateTime @1751037581 {#128285 : 2025-06-27 17:19:41.0 Europe/Paris (+02:00) } #updatedAt: DateTime @1754606304 {#128319 : 2025-08-08 00:38:24.0 Europe/Paris (+02:00) } #enabled: true #translations: Doctrine\ORM\PersistentCollection {#128306 …} #translationsCache: [ "en_US" => App\Entity\Product\ProductTranslation {#128406 #locale: "en_US" #translatable: App\Entity\Product\Product {#128312} #id: 29549 #name: "IEEE 528:1984" #slug: "ieee-528-1984-ieee00000778-240287" #description: """ New IEEE Standard - Inactive-Withdrawn.<br />\n Withdrawn Status. Terms and definitions relating to inertial sensors are presented. Usage as understood by the inertial sensor 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 sensor technology.<br />\n \t\t\t\t<br />\n Terms and definitions relating to inertial sensors are presented. Usage as understood by the inertial sensor 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 sensor technology. """ #metaKeywords: null #metaDescription: null #shortDescription: "IEEE Standard Inertial Sensor Terminology" -notes: "Inactive-Withdrawn" } ] #currentLocale: "en_US" #currentTranslation: null #fallbackLocale: "en_US" #variantSelectionMethod: "match" #productTaxons: Doctrine\ORM\PersistentCollection {#128304 …} #channels: Doctrine\ORM\PersistentCollection {#128297 …} #mainTaxon: Proxies\__CG__\App\Entity\Taxonomy\Taxon {#7308 …} #reviews: Doctrine\ORM\PersistentCollection {#128301 …} #averageRating: 0.0 #images: Doctrine\ORM\PersistentCollection {#128299 …} -supplier: Proxies\__CG__\App\Entity\Supplier\Supplier {#7422 …} -subscriptionCollections: Doctrine\ORM\PersistentCollection {#128270 …} -apiLastModifiedAt: DateTime @1754517600 {#128271 : 2025-08-07 00:00:00.0 Europe/Paris (+02:00) } -lastUpdatedAt: DateTime @1578006000 {#128313 : 2020-01-03 00:00:00.0 Europe/Paris (+01:00) } -author: "" -publishedAt: DateTime @442710000 {#128320 : 1984-01-12 00:00:00.0 Europe/Paris (+01:00) } -releasedAt: null -confirmedAt: null -canceledAt: DateTime @691887600 {#128278 : 1991-12-05 00:00:00.0 Europe/Paris (+01:00) } -edition: null -coreDocument: "528" -bookCollection: "" -pageCount: 16 -documents: Doctrine\ORM\PersistentCollection {#128310 …} -favorites: Doctrine\ORM\PersistentCollection {#128308 …} } +label: "Historical" +icon: "historical" -mostRecentAttributeCode: "most_recent" -localeContext: Sylius\Component\Locale\Context\CompositeLocaleContext {#1833 …} } |
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