The results of fly-by-wire programs are outlined and a description of the B-47 fly-by-wire flight tests is given. Papers presented discuss the potential application of fly-by-wire for advanced fighters, large strategic bombers, and helicopters and outline the philosophy of redundancy, digital computation, handling qualities criterion and pilot acceptance as related to fly-by-wire flight control systems. (Author)
Proceedings of the Fly-by-Wire Flight Control System Conference, 16-17 December 1968
1969
282 pages
Report
No indication
English
Aircraft , Flight control systems , Symposia , Electric wire , Jet bombers , Jet fighters , Helicopters , Handling , Acceptability , Redundant components , Analog computers , Synchros , Signals , Digital computers , Vertical takeoff aircraft , Man machine systems , Fly by wire flight control systems , Automatic , Control , Control systems , B-47 aircraft , Closed loop systems , V-4 aircraft , Xv-4b aircraft
Anthena V-118B, Flight 109 (12 December 1968)
NTIS | 1969
|Proceedings of WODCON : 1968 ; World Dredging Conference
TIBKAT | 1968
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