Discrete-time Lpv Controller for Robust Missile Autopilot Design

نویسندگان

  • D. Farret
  • G. Duc
  • J. P. Harcaut
چکیده

This paper proposes a method to obtain a discrete-time LPV (Linear Parameter Varying) controller for a non-linear system represented with the LFT (Linear Fractional Transformation) framework. This synthesis can be integrated into a loop-shaping/LPV approach to obtain a discrete gain-scheduled control law. A detailed application of this method is here performed with a classical example of non-linear missile pitch-axis control. Copyright © 2002 IFAC

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تاریخ انتشار 2002