SAE ARP5287
Current
The latest, up-to-date edition.
Optical Measurement Procedures for Airborne Head Up Display (HUD)
Hardcopy , PDF
English
04-01-2008
1 SCOPE
2 REFERENCES
2.1 Applicable Documents
2.2 Related Publications
2.3 Definitions
3 GENERAL REQUIREMENTS
3.1 Laboratory Standard Measurement Conditions
3.2 Laboratory Standards
3.3 Measurement Equipment
4 MEASUREMENT PROCEDURES
4.1 HUD Angular Measurements
4.2 Field of View (FOV) Measurements
4.3 HUD Eyebox Size Measurements
4.4 Symbol Positioning Accuracy
4.5 Display Drift
4.6 Line Width
4.7 Display Jitter
4.8 Binocular Parallax
4.9 HUD Luminance
4.10 HUD Combiner Transmissivity
4.11 Minimum HUD Luminance
4.12 Automatic Luminance Control
4.13 Combiner Head Injury Criteria (HIC)
4.14 Raster Contrast Variation
4.15 Raster Low Level Luminance
4.16 Raster Luminance Uniformity
4.17 Combiner Induced Real World Distortion and Parallax
Errors
4.18 Secondary Display Images
4.19 Color Registration
5 AS8055 TO ARP5287 CROSS REFERENCE
Includes procedures for measuring the optical performance of airborne binocular Head Up Displays (HUDs).
DocumentType |
Standard
|
Pages |
17
|
PublisherName |
SAE International
|
Status |
Current
|
Supersedes |
This SAE Aerospace Recommended Practice (ARP) contains methods used to measure the optical performance of airborne binocular Head Up Displays (HUDs). This document covers methods for conformal and non-conformal HUD systems that are intended for use in the cockpit by the pilot or copilot. The focus of this document is on displays that generate the HUD information using a cathode ray tube (CRT), however, the majority of the methods can be applied to other display technologies. These measurement methods are provided for testing to the requirements of AS8055.This document does not address measurement methods for sensor imaging systems, or displays worn by the pilot (goggles, helmet mounted displays).
SAE ARP 4260 : 2014 | PHOTOMETRIC AND COLORIMETRIC MEASUREMENT PROCEDURES FOR AIRBORNE ELECTRONIC FLAT PANEL DISPLAYS |
RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
SAE J1330_201409 | Photometry Laboratory Accuracy Guidelines |
MIL-STD-1787 Revision B:1996 | AIRCRAFT DISPLAY SYMBOLOGY |
SAE ARP4032B | Human Engineering Considerations in the Application of Color to Electronic Aircraft Displays |
SAE ARP 4155 : 1997 | HUMAN INTERFACE DESIGN METHODOLOGY FOR INTEGRATED DISPLAY SYMBOLOGY |
MIL-STD-1241 Revision A:1967 | Optical Terms and Definitions |
MIL-HDBK-87213 Revision A:2005 | Electronically / Optically Generated Airborne Displays |
SAE AS8055A | Minimum Performance Standard for Airborne Head Up Display (HUD) |
MIL-STD-1295 Revision A:1984 | HUMAN FACTORS ENGINEERING DESIGN CRITERIA FOR HELICOPTER COCKPIT ELECTRO-OPTICAL DISPLAY SYMBOLOGY |
SAE ARP4102/8A | Flight Deck Head-Up Displays |
SAE ARP 1874 : 1988 | DESIGN OBJECTIVES FOR CRT DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT |
SAE AS8034B | Minimum Performance Standard for Airborne Multipurpose Electronic Displays |
SAE ARP 4256 : 2001 | DESIGN OBJECTIVES FOR LIQUID CRYSTAL DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT |
SAE ARP1782B | Photometric and Colorimetric Measurement Procedures for Airborne Direct View CRT Displays |
FAA AC 20-57 : A | AUTOMATIC LANDING SYSTEMS (ALS) |
SAE ARP 4103 : 2014 | FLIGHT DECK LIGHTING FOR COMMERCIAL TRANSPORT AIRCRAFT |
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