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.
Ground and flight test experience with a triple redundant digital fly by wire control system
1981-02-01
Conference paper
No indication
English
Triple-Triple Redundant 777 Primary Flight Computer
British Library Conference Proceedings | 1996
|Digital Fly-By-Wire Flight Control Validation Experience
NTRS | 1978
|