SAE ARP 4260-1998

Photometric and colorimetric measurement procedures for airborne flat panel displays

SAE ARP 4260-1998 发布历史

The SAE Aerospace Recommended Practice (ARP) contains methods used to measure the optical performance of airborne flat panel display (FPD) systems. The methods described are specific to the direct view, liquid crystal matrix (x-y addressable) display technology used on aircraft flight decks. The focus of this document is on active matrix, liquid crystal displays (LCD), however, the majority of the procedures can be applied to other display technologies. The document covers monochrome and color LCD operation in the transmissive mode within the visual spectrum (the wavelength range of 380 to 780 nm). These procedures are adaptable to reflective and transflective displays paying special attention to the source illumination geometry. Generally, the procedures describe manual single point measurements. The individual procedures may be readily incorporated into automated testing equipment (ATE) or other automated environments. This also includes, but is not limited to Fourier scopes and video imaging devices. This document defines three classes of tests. Each class of test is applicable to the different phases of a products life (e.g., engineering development (Class 1), production/quality assurance (Class 2) and service/flight readiness (Class 3)). The test requirements for each of these phases differ and hence the test procedures for each test class may differ. Each procedure in this document is Class 1 unless otherwise stated

SAE ARP 4260-1998由美国机动车工程师协会 US-SAE 发布于 1998-11-01。

SAE ARP 4260-1998在国际标准分类中归属于: 49.090 机上设备和仪器。

SAE ARP 4260-1998的历代版本如下：

• 1998年11月01日 SAE ARP 4260-1998

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标准号

SAE ARP 4260-1998

发布日期

1998年11月01日

实施日期

废止日期

无

国际标准分类号

49.090

发布单位

US-SAE

代替标准

SAE ARP 4260A-2009

适用范围

The SAE Aerospace Recommended Practice (ARP) contains methods used to measure the optical performance of airborne flat panel display (FPD) systems. The methods described are specific to the direct view, liquid crystal matrix (x-y addressable) display technology used on aircraft flight decks. The focus of this document is on active matrix, liquid crystal displays (LCD), however, the majority of the procedures can be applied to other display technologies. The document covers monochrome and color LCD operation in the transmissive mode within the visual spectrum (the wavelength range of 380 to 780 nm). These procedures are adaptable to reflective and transflective displays paying special attention to the source illumination geometry. Generally, the procedures describe manual single point measurements. The individual procedures may be readily incorporated into automated testing equipment (ATE) or other automated environments. This also includes, but is not limited to Fourier scopes and video imaging devices. This document defines three classes of tests. Each class of test is applicable to the different phases of a products life (e.g., engineering development (Class 1), production/quality assurance (Class 2) and service/flight readiness (Class 3)). The test requirements for each of these phases differ and hence the test procedures for each test class may differ. Each procedure in this document is Class 1 unless otherwise stated

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