STUDY OF A SAFETY MARGIN SYSTEM FOR POWERED-LIFT STOL AIRCRAFT
A study was conducted to explore the feasibility of a safety margin system for powered-lift aircraft which require a backside piloting technique. The objective of the safety margin system was to present multiple safety margin criteria as a single variable which could be tracked manually or automatically and which could be monitored for the purpose of deriving safety margin status. The study involved a pilot-in-the-loop analysis of several safety margin system concepts and a simulation experiment to evaluate those concepts which showed promise of providing a good solution. A system was ultimately configured which offered reasonable compromises in controllability, status information content, and the ability to regulate the safety margin at some expense of the allowable low speed flight path envelope.
Systems Technology, Incorporated13766 South Hawthorne Boulevard
Hawthorne, CA United States 90250
- Heffley, R K
- Jewell, W F
- Publication Date: 1978-5
- Pagination: 160 p.
- TRT Terms: Automatic control; Aviation safety; Flight control systems; Interoperability; Manual control; Safety; Standards; STOL aircraft; Systems engineering
- Uncontrolled Terms: Aircraft safety; Safety standards
- Old TRIS Terms: Jet lift; Short takeoff aircraft; Systems compatibility
- Subject Areas: Aviation; Safety and Human Factors; Vehicles and Equipment;
- Accession Number: 00181656
- Record Type: Publication
- Source Agency: National Technical Information Service
- Report/Paper Numbers: NASA-CR-152139 Final Rpt.
- Contract Numbers: NAS2-9418
- Files: TRIS
- Created Date: Oct 31 1979 12:00AM