The development of flight control systems using classical control techniques is a costly and time-consuming process. This paper shows how to use genetic algorithm (GA) and modern control techniques to determine the control parameters of the flight control law within the classical structure. An example of designing longitudinal flight control law with the proposed method is presented. The designed flight control law be simulated on a 6 degree-of-freedom nonlinear model of the aircraft.
Fixed structure flight control law design based on genetic algorithm
2006
4 Seiten, 7 Quellen
Aufsatz (Konferenz)
Englisch
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