Abstract The laws of lateral motion control without data on the roll angle are proposed for aircraft with a single plane of symmetry. A procedure for analytical selection of the optimal gain in the aileron and rudder channels is proposed. The results of simulating the aircraft-autopilot system are presented.
Aircraft lateral-directional control without a roll command in the autopilot
Russian Aeronautics (Iz VUZ) ; 57 , 2 ; 134-140
2014-04-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Aircraft lateral-directional control without a roll command in the autopilot
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