Design and test experience with a triply redundant digital fly-by-wire control system
- 16 August 1976
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Balanced functional design of automatic digital flight control systemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Digital flight control systems - Considerations in implementation and acceptancePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Flight test of a digital guidance and control system in a DC-10 aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Design and flight experience with a digital fly-by-wire control system using Apollo guidance system hardware on an F-8 aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972