Fly-By-Wire Flight Control System Design Considerations for Fighter Aircraft

751046

02/01/1975

Event
Aerospace Engineering and Manufacturing Meeting
Authors Abstract
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.
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DOI
https://doi.org/10.4271/751046
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.
Additional Details
Publisher
Published
Feb 1, 1975
Product Code
751046
Content Type
Technical Paper
Language
English