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A composite sliding mode autopilot design
by Qunli Xia, Jingju Zhu, Zaikang Qi
International Journal of Modelling, Identification and Control (IJMIC), Vol. 9, No. 1/2, 2010

 

Abstract: Sliding mode control has been applied to the design of many missile autopilots. In this paper, a control method with the primary feedback being proportional to the switching is developed for eliminating the disturbance effect due to model uncertainty. With this control method, a sliding mode autopilot is analysed. Then, a composite sliding mode control strategy is discussed to reduce the switching frequency. Numerical simulation results show a good performance of the composite control system.

Online publication date: Thu, 01-Apr-2010

 

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