Nonlinear Discrete-time Design Methods for Missile Flight Control Systems

  • P. K. Menon
  • G. D. Sweriduk
  • S. S. Vaddi
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Publication date
October 2016

Abstract

Discrete-time designs of flight control systems are required for implementation on missile-borne computers. While extensive literature is available on linear discrete-time control system design methods, nonlinear discrete-time control system design techniques have not been discussed to the same degree. This paper presents three nonlinear, discrete-time control system design methods. These are the discrete-time feedback linearization method, discrete-time state-dependent Riccatti equation method, and the discrete-time recursive backstepping technique. Nonlinear missile autopilot design for a conventional missile and an integrated guidance-control system design for a moving mass actuated missile are given as illustrative examples. I

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