Fly-By-Wire Flight Control System Design Considerations for Fighter Aircraft
751046
02/01/1975
- Event
- Content
- The application of fly-by-wire flight control systems in fighter aircraft influences the basic design of the aircraft and requires special attention to certain design characteristics of the control system. The use of control-configured vehicle concepts for performance benefits makes fly-by-wire a logical choice. Redundancy management, protection against power loss, lightning protection and controller selection are prime design factors to be considered. Flight testing of the YF-16 aircraft has demonstrated excellent performance and operating characteristics of its fly-by-wire flight control system.
- Pages
- 7
- Citation
- Livingston, E., "Fly-By-Wire Flight Control System Design Considerations for Fighter Aircraft," SAE Technical Paper 751046, 1975, https://doi.org/10.4271/751046.