NASA NTRS · 19880000218
Development Of A Digital Flight-Control System
Abstract
Feed-forward control path includes inversion of model of the aircraft. Report describes concept, development, tests of digital flight-control system for vertical-attitude-takeoff-and-landing aircraft. System based in airborne digital computer. Combines control of attitude and thrust in unified system for operation over full coupled ranges of velocity, altitude, attitude, and acceleration.
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Smith, G. Allan, Meyer, George. 1988-04-01. Development Of A Digital Flight-Control System. https://ntrs.nasa.gov/citations/19880000218
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