SAE ARP5589
Current
The latest, up-to-date edition.
Human Engineering Considerations for Design and Implementation of Perspective Flight Guidance Displays
05-01-2005
FOREWORD
ACKNOWLEDGEMENT
1 SCOPE
1.1 Purpose
2 REFERENCES
2.1 Applicable Documents
2.1.1 SAE Publications
2.1.2 FAA Publications
2.1.3 EUROCAE Publications
2.2 Other Applicable References
2.3 Regulatory Publications
2.4 Related Publications
2.5 Definition of Terms
2.6 Acronyms and Abbreviations
3 ASSUMPTIONS
4 DESIGN REQUIREMENTS AND OBJECTIVES
4.1 Design Requirements
4.2 Design Objectives
5 CONCEPT OF PERSPECTIVE DISPLAYS
5.1 Basic Philosophy - Why Perspective Guidance?
5.2 Underlying Rationale
5.3 Advantages
5.4 Potential Disadvantages
5.5 Issues
5.6 Data Integration versus Workload Reduction
5.7 Minimize Mental Rotations
5.8 Preview
6 PFGD DESIGN RECOMMENDATIONS
6.1 Display Characteristics
6.1.1 Field of Regard
6.1.2 Frame of Reference
6.2 Elements of 3-D Data Presentation
6.2.1 Spatial Orientation
6.2.2 Pathway Depiction
6.2.3 Control Task
6.2.4 Trajectory Guidance
6.3 Flight Crew Interface Requirements
6.3.1 Mode Change
6.3.2 PFGD Differentiation
6.3.3 Declutter Mode(s)
6.4 PFGD Elements and Information Content
6.4.1 Presentation of Pathway
6.5 Planned/Geo-referenced Mode
6.5.1 Geo-referenced Track Guidance
6.5.2 Geo-referenced Pathway Reacquisition
6.6 Pathway Guidance Augmentation -
Flight Director/Auto-Flight Coupled Modes
6.6.1 Examples of Design Requirements
6.7 Other Information Integration in the 3-D World
6.7.1 Terrain
6.7.2 Traffic
6.7.3 Weather
6.7.4 Restricted/Special Use Airspace
6.7.5 Obstacles
6.8 2-D Overlay Symbology/Instruments Not Directly Related
to the 3-D World
6.8.1 Aeroperformance Data
APPENDIX A REPRESENTATIVE PERSPECTIVE DISPLAY(S)
APPENDIX B SUPPORTING DATA - PERSPECTIVE FLIGHT GUIDANCE
PHILOSOPHY
APPENDIX C SUPPORTING DATA - FLIGHT DIRECTOR MODES
Focuses on perspective flight displays with or without guidance and is intended for flight deck display applications.
DocumentType |
Standard
|
PublisherName |
SAE International
|
Status |
Current
|
The document focuses on perspective flight displays with or without guidance and is intended for flight deck display applications. Further, this document does not directly address the presence or absence of background information, e.g., synthetic and/or enhanced imagery. Such issues are addressed in a separate E/SVS document.Since this document provides recommendations, the guidance is provided in the form of “should” statements as opposed to the “shall” statements that appear in standards and regulations. When “shall” statements are used, the regulation or standard is referenced (where applicable).
FAA AC 20-167 : 2016 | AIRWORTHINESS APPROVAL OF ENHANCED VISION SYSTEM, SYNTHETIC VISION SYSTEM, COMBINED VISION SYSTEM, AND ENHANCED FLIGHT VISION SYSTEM EQUIPMENT |
SAE ARP1161A | CREW STATION LIGHTING - COMMERCIAL AIRCRAFT |
SAE ARP 4260 : 2014 | PHOTOMETRIC AND COLORIMETRIC MEASUREMENT PROCEDURES FOR AIRBORNE ELECTRONIC FLAT PANEL DISPLAYS |
RTCA DO 200B : 2015 | STANDARDS FOR PROCESSING AERONAUTICAL DATA |
FAA AC 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
SAE AS264F | INSTRUMENT AND COCKPIT LIGHTING FOR COMMERCIAL TRANSPORT AIRCRAFT |
SAE ARP 4107 : 2008 | AEROSPACE GLOSSARY OF HUMAN FACTORS ENGINEERS |
RTCA DO-201A : 2000 | STANDARDS FOR AERONAUTICAL INFORMATION |
SAE ARP 268 : 1994 | LOCATION AND ACTUATION OF FLIGHT DECK CONTROLS FOR TRANSPORT |
FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
SAE ARP 1068 : 1994 | FLIGHT DECK INSTRUMENTATION, DISPLAY CRITERIA AND ASSOCIATED CONTROLS FOR TRANSPORT AIRCRAFT |
SAE ARP4032B | HUMAN ENGINEERING CONSIDERATIONS IN THE APPLICATION OF COLOR TO ELECTRONIC AIRCRAFT DISPLAYS |
SAE ARP 4102/4 : 1988 | FLIGHT DECK ALERTING SYSTEM (FAS) |
SAE ARP 571 : 1994 | FLIGHT DECK CONTROLS AND DISPLAYS FOR COMMUNICATION AND NAVIGATION EQUIPMENT FOR TRANSPORT AIRCRAFT |
SAE ARP 4101 : 1988 | FLIGHT DECK LAYOUT AND FACILITIES |
SAE ARP 4105 : 2012 | ABBREVIATIONS, ACRONYMS, AND TERMS FOR USE ON THE FLIGHT DECK |
FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
FAA AC 120-29 : 0 | CRITERIA FOR APPROVAL OF CATEGORY 1 AND CATEGORY 2 WEATHER MINIMA FOR APPROACH |
SAE ARP 4033 : 1995 | PILOT-SYSTEM INTEGRATION |
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 5289 : 2011 | ELECTRONIC AERONAUTICAL SYMBOLS |
SAE ARP 5119 : 2013 | LOCATION OF AND DISPLAY SYMBOLOGY REQUIREMENTS FOR HEAD-DOWN ELECTRONIC FLIGHT DISPLAYS FOR STEEP IMC APPROACHES |
SAE ARP 4153 : 1988 | HUMAN INTERFACE CRITERIA FOR COLLISION AVOIDANCE SYSTEMS IN TRANSPORT AIRCRAFT |
SAE ARP 4102/7 : 1988 | ELECTRONIC DISPLAYS |
SAE ARP 4101/2 : 1989 | PILOT VISIBILITY FROM THE FLIGHT DECK |
SAE AS8034B | MINIMUM PERFORMANCE STANDARD FOR AIRBORNE MULTIPURPOSE ELECTRONIC DISPLAYS |
SAE AS 425 : 1985 | NOMENCLATURE AND ABBREVIATIONS FOR USE ON THE FLIGHT DECK |
SAE ARD 50018 : 1995 | THE INTEGRATION OF VERTICAL FLIGHT AIRCRAFT INTO THE NATIONAL AIRSPACE SYSTEM |
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 COLORMETRIC MEASUREMENT PROCEDURES FOR AIRBORNE DIRECT VIEW CRT DISPLAYS |
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