The problem of synthesizing the pitch angle control system with the angle of attack limiting channel is considered. The problem of matching the trajectories of the system of the pitch angle control mode and the angle of attack limitation mode is discussed. An approach is proposed based on using a generalized characteristic of the system, which ensures the matching the states at an arbitrary moment of change of its operation mode.
Synthesis of Pitch Angle Control System with Angle of Attack Limiting Channel
Russ. Aeronaut.
Russian Aeronautics ; 63 , 1 ; 25-32
2020-01-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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