Back to Search
Start Over
Ground and flight test experience with a triple redundant digital fly by wire control system
- Source :
- NASA. Langley Research Center Advan. Aerodyn. and Active Controls.
- Publication Year :
- 1981
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1981.
-
Abstract
- A triplex digital fly by wire flight control system was developed and installed in an F-8C aircraft to provide fail operative, full authority control. Hardware and software redundancy management techniques were designed to detect and identify failures in the system. Control functions typical of those projected for future actively controlled vehicles were implemented.
- Subjects :
- Aircraft Stability And Control
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Journal :
- NASA. Langley Research Center Advan. Aerodyn. and Active Controls
- Publication Type :
- Report
- Accession number :
- edsnas.19810010480
- Document Type :
- Report