• 제목/요약/키워드: BTT Missile

검색결과 11건 처리시간 0.015초

$H_2/H_{\infty}$ 혼합 제어기를 이용한 고속 비행체의 자동조정장치 설계 (Design of Autopilot for High Velocity Flight Vehicles using Mixed $H_2/H_{\infty}$ Controller)

  • 이종성
    • 대한전자공학회:학술대회논문집
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    • 대한전자공학회 2005년도 추계종합학술대회
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    • pp.1297-1300
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    • 2005

  • 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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