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Nonlinear system partial linearization and its application to flight control
Pages: 13-22+39
Year: Issue:  4
Journal: Aerospace Control

Keyword:  Nonlinear systemFlight control systemGuidanceSability;
Abstract: The paper presents and researchs the problem of partial linearization of anonlinear system based on the design concept of lineatization of nonlinear system.The suffi-cient and necessary condition that a nonline system can partially be linearized is given.On thebase,the design problem of the attitude control system of a certain vehicle is researched and itscontrol law is given out.Finally,the correctness of the method presented in this paper is veri-fied by nvmerieal value simulation.
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