To a problem of aircraft control system design with given dynamic parameters |
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Authors: | V I Garkushenko P A Lazareva |
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Institution: | 1.Tupolev Kazan National Research Technical University,Kazan Tatarstan,Russia |
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Abstract: | In the design of an aircraft at the stage of selecting its geometrical parameters, a method is proposed for evaluating the performance capabilities of manual control to ensure the quality of a given flight stabilization mode. The attainability of the given aircraft-pilot dynamic properties is evaluated by a frequency-domain method for permissible values of the aircraft and the pilot model parameters. The quality of the manual control for the longitudinal motion of the aircraft is evaluated. |
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