Design of Autopilot for High Velocity Flight Vehicles using Mixed $H_2/H_{\infty}$ Controller

$H_2/H_{\infty}$ 혼합 제어기를 이용한 고속 비행체의 자동조정장치 설계

  • Published : 2005.11.26

Abstract

In this study the gradient method is used to design a mixed $H_2/H_{\infty}$ controller. It is verified by an example that is BTT missile. We expect through the results of this study that gradient method can be easily applied to diverse optimization problems.

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