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Design Freedom Offered by Fly-by-Wire
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English
Abstract
Fly-By-Wire offers the designer flexibility in mechanizing the manual flight control system and makes possible potential CCV performance benefits because more complex functions can be implemented. The full potential of FBW and CCV can only be achieved by incorporating these concepts in the initial design phase of a new airplane. Greater benefits are obtained in several areas when applying FBW and CCV simultaneously.
Authors
Citation
Newberry, C., "Design Freedom Offered by Fly-by-Wire," SAE Technical Paper 751044, 1975, https://doi.org/10.4271/751044.Also In
References
- Sutherland, F/L, J.P. “Fly-By-Wire Control Systems” SAE-18 Aerospace Vehicle Flight Control Committee Boston, Mass. 10 August 1967
- AFFDL-TR-74-92 1 “B-52 CCV Program Summary” March 1975
- AFFDL-TR-73-83 “Control Configured Vehicle Ride Control System, B-52 Control System Analysis, Synthesis, and Design” July 1973
- McKenzie, J.R. “B-52 Control Configured Vehicles Ride Control Analysis and Flight Test” AIAA Paper No. 73-782
- Felt, L. Hodges, G.E. Roger, K.L. “Active Flutter Suppression - A Flight Test Demonstration” AIAA Paper No. 74-402
- Hodges, G.E. McKenzie, J.R. “B-52 Control Configured Vehicles Maneuver Load Control System Analysis and Flight Test Results” AIAA Paper No. 75-72
- Walker, Stephen A. “Design of a Control Configured Tanker Aircraft” Symposium on Advanced Control Technology National Aeronautics and Space Administration Los Angeles, Calif. 9-11 July 1974