Abstract
Considering the pitch channel simplified model of supersonic missile system, a integral type of sliding surface is constructed with the error of overload and the integration of error and the angle speed signal. Base on the linear sliding mode, a simple PS adaptive integral sliding mode controller is designed In order to improve the performance of the proposed method, two improvements also proposed. Finally, a hybrid PISS adaptive control is formed which contains proportion control, integration control, the sign function and soft function.
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