NASA/RAE Collaboration on Nonlinear Control Using the F-8C Digital Fly-by-wire Aircraft1983 - 20 pages |
Common terms and phrases
actuators Ames Research Center angle of attack augmented vehicle RAV baseline loop baseline system CADRE control laws CADRE system chase aircraft command prefilter control-law computer Corbin damping deg/sec delay developed by RAE digital research downlink rate check downlink telemetry Dryden Flight Research ELEVATOR DEMAND experimental control F-8C DFBW F-8C digital fly-by-wire F-8C RAV feed-forward Final Software Flight Research Facility FORTRAN gain scheduling Gill ground-based computer high-gain implementation integral gain interface iron-bird simulation lift force maneuver Memo FS NASA noise filter on-board system operation overshoot control parameters PILOT DEMAND pilot input pilot rating PITCH RATE pitch-rate controller pitch-rate response pitching moment RAE Tech rate-limit RAV command RAV downmode RAV engagement RAV facility RAV ground computer RAV system remotely augmented vehicle Royal Aircraft Establishment sensor signal single-string simplex subroutines uplink and downlink variable variable-gain algorithm variable-gain control laws VICTOR error VICTOR gearing VICTOR loop VICTOR system VICTOR-E algorithm zero