Abstract The laws of longitudinal motion control without data on the pitch angle are proposed. A procedure for analytical selection of the optimal gain in the elevator channel is proposed. The results of simulating the aircraft-autopilot system are presented.
Aircraft longitudinal control without a pitch command in the autopilot
Russian Aeronautics (Iz VUZ) ; 57 , 4 ; 361-367
2014-10-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Aircraft longitudinal control without a pitch command in the autopilot
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