Application of feedback linearization and continuous sliding mode control to a nonlinear helicopter model

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Abstract

A continuous sliding mode control method based on feedback linearization is presented to realize the coupling control for a MIMO nonlinear system such as helicopter. A discontinuous sliding mode control can be changed into a continuous one by extending the nonlinear system. Thus the system robustness can be enhanced. The control system for the vertical flight mode of a helicopter is designed. Simulation results are in agreement with the theoretical analysis results and the system can track the given input.

Original languageEnglish
Pages (from-to)378-381
Number of pages4
JournalXibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University
Volume18
Issue number3
StatePublished - Aug 2000

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