SAE ARP5677
Current
The latest, up-to-date edition.
Human Engineering Considerations for Airborne Implementation of Enhanced Synthetic Vision Systems
18-12-2012
1. SCOPE
2. REFERENCES
3. ASSUMPTIONS
4. DESIGN OBJECTIVES
5. DISPLAY METHOD
6. ESVS DESIGN CONSIDERATIONS
7. SENSORS/IMAGE SOURCE
8. WORKLOAD IMPLICATIONS
9. SYSTEM SAFETY
10. TRAINING FOR USE
11. SYSTEM PERFORMANCE TESTING
12. NOTES
APPENDIX A - BIBLIOGRAPHY RELATED TO
HUMAN FACTORS IN DESIGN
AND IMPLEMENTATION OF
ESVS SYSTEMS
The scope of this document is limited to Enhanced Synthetic Vision Systems ESVS human factors considerations and requirements in comprehension, interpretation and application of imagery and integrated symbology in Enhanced (sensor) and Synthetic (database) Vision Systems in aircraft.
DocumentType |
Standard
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PublisherName |
SAE International
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Status |
Current
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The scope of this document is limited to Enhanced Synthetic Vision Systems ESVS human factors considerations and requirements in comprehension, interpretation and application of imagery and integrated symbology in Enhanced (sensor) and Synthetic (database) Vision Systems in aircraft. Any overlap into logic problems or hardware/software design should be considered to be incidental to the human factors issues. Where the performance characteristics of specific technologies are relevant they will be identified, and where performance criteria are relevant to specific intended functions/use they will be identified. From a regulatory view, intended function (Guidance or Information/Situation Awareness support) has a tremendous effect upon the design of an ESV System. However from a Human Engineering standpoint, the information on a display must be discernible and comprehensible to the human operator in both cases and differences may be primarily in information content (required to support a specific task).This document attempts to be independent of candidate technologies and concentrate on human interface criteria.Consideration of NVG use in a cockpit equipped with ESVS is beyond the scope of this document, but it should be noted that there will be significant integration/interaction issues such as black level limits and use of DTED data simultaneous with NVS. This document does not include consideration of detection and/or display of air targets or integration of systems such as TCAS.
FAA AC 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
FAA AC 20-167 : 2016 | AIRWORTHINESS APPROVAL OF ENHANCED VISION SYSTEM, SYNTHETIC VISION SYSTEM, COMBINED VISION SYSTEM, AND ENHANCED FLIGHT VISION SYSTEM EQUIPMENT |
SAE ARP6023 | Human Engineering Considerations for Implementing Enhanced Synthetic Vision Systems in Vertical Flight Capable Platforms |
RTCA DO 200B : 2015 | STANDARDS FOR PROCESSING AERONAUTICAL DATA |
FAA AC 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
SAE ARP4107 | AEROSPACE GLOSSARY FOR HUMAN FACTORS ENGINEERS |
FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
SAE ARP 1068 : 1994 | FLIGHT DECK INSTRUMENTATION, DISPLAY CRITERIA AND ASSOCIATED CONTROLS FOR TRANSPORT AIRCRAFT |
SAE AS 580 : 1994 | PILOT VISIBILITY FROM THE FLIGHT DECK DESIGN OBJECTIVES FOR COMMERCIAL TRANSPORT AIRCRAFT |
FAA AC 90-106 : 2017 | ENHANCED FLIGHT VISION SYSTEMS |
FAA AC 20-167 : 2016 | AIRWORTHINESS APPROVAL OF ENHANCED VISION SYSTEM, SYNTHETIC VISION SYSTEM, COMBINED VISION SYSTEM, AND ENHANCED FLIGHT VISION SYSTEM EQUIPMENT |
SAE ARP4032B | Human Engineering Considerations in the Application of Color to Electronic Aircraft Displays |
SAE ARP 571 : 1994 | FLIGHT DECK CONTROLS AND DISPLAYS FOR COMMUNICATION AND NAVIGATION EQUIPMENT FOR TRANSPORT AIRCRAFT |
SAE ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
SAE ARD 50019 : 1995 | HUMAN ENGINEERING ISSUES FOR ENHANCED VISION SYSTEMS |
SAE ARP5056 | Flight Crew Interface Considerations in the Flight Deck Design Process for Part 25 Aircraft |
SAE ARP 4155 : 1997 | HUMAN INTERFACE DESIGN METHODOLOGY FOR INTEGRATED DISPLAY SYMBOLOGY |
RTCA DO 309 : 2008 | MINIMUM OPERATIONAL PERFORMANCE STANDARDS (MOPS) FOR HELICOPTER TERRAIN AWARENESS AND WARNING SYSTEM (HTAWS) AIRBORNE EQUIPMENT |
FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
SAE AS8055A | Minimum Performance Standard for Airborne Head Up Display (HUD) |
SAE AIR1093A | Numeral, Letter and Symbol Dimensions for Aircraft Instrument Displays |
RTCA DO 276 : C2015 | USER REQUIREMENTS FOR TERRAIN AND OBSTACLE DATA |
MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
FAA AC 25.1309-1 : 0 | SYSTEM DESIGN AND ANALYSIS |
SAE ARP 1874 : 1988 | DESIGN OBJECTIVES FOR CRT DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT |
SAE ARP 5288 : 2001 | TRANSPORT CATEGORY AIRPLANE HEAD UP DISPLAY (HUD) SYSTEMS |
RTCA DO 315 : B2011 | MINIMUM AVIATION SYSTEM PERFORMANCE STANDARDS (MASPS) FOR ENHANCED VISION SYSTEMS, SYNTHETIC VISION SYSTEMS, COMBINED VISION SYSTEMS AND ENHANCED FLIGHT VISION SYSTEMS |
SAE AS8034B | Minimum Performance Standard for Airborne Multipurpose Electronic Displays |
ISO 9241-8:1997 | Ergonomic requirements for office work with visual display terminals (VDTs) Part 8: Requirements for displayed colours |
SAE ARP 4256 : 2001 | DESIGN OBJECTIVES FOR LIQUID CRYSTAL DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT |
SAE ARP 4102 : 1988 | FLIGHT DECK PANELS, CONTROLS, AND DISPLAYS |
SAE ARP1782B | Photometric and Colorimetric Measurement Procedures for Airborne Direct View CRT Displays |
RTCA DO 341 : 2012 | MINIMUM AVIATION SYSTEM PERFORMANCE STANDARDS (MASPS) FOR AN ENHANCED FLIGHT VISION SYSTEM TO ENABLE ALL-WEATHER APPROACH, LANDING AND ROLL-OUT TO A SAFE TAXI SPEED |
FAA AC 25.1322-1 : 2010 | FLIGHTCREW ALERTING |
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