• Shopping Cart
    There are no items in your cart

SAE ARP5677

Current

Current

The latest, up-to-date edition.

Human Engineering Considerations for Airborne Implementation of Enhanced Synthetic Vision Systems

Published date

18-12-2012

Sorry this product is not available in your region.

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
PublisherName
SAE International
Status
Current

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

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.