• 한국정밀공학회지
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• 제12권1호
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• pp.78-86
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• 1995

$H_{\infty}$ Controller of seeker scan-loop is designed using LSDP proposed by McFarlane. The performance and robustness of $H_{\infty}$ controller are analyzed using robustness theorems by Lehtomaki and compared with those of the LQG/LTR controller. Especially, structured singular value .mu. -test of Doyle is used to evaluate robust performance of seeker scan-loop. It is demonstated that seeker scan-loop by $H_{\infty}$ controller is very robust to model uncertainties described by additive and multiplicative perturbations.

• 한국정밀공학회지
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• 제14권11호
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• pp.102-109
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• 1997

A two-degree-of freedom (TDF) $H_{\infty}$controller for a seeker scan loop is presented for the purpose of improving scanning performances. The perturbed plant model is characterized via the normalized coprime factorization. The TDF $H_{\infty}$controller is designed based on the loop shaping design procedure and model matching approach, and its performances are evaluated and compared with those of a previous work. It is demonstrated that the proposed TDF $H_{\infty}$controller is more effective to the control of the seeker scan loop than the previous controller.oller.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 춘계학술대회논문집
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• pp.251-256
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• 2000

This paper presents dynamic modeling and controller design of a tracked vehicle installed with the double-rod type ERSU(electro-rheological suspension unit). A 16 DOF(degree-of-freedom) model for the tracked vehicle is established by Lagrangian method. After showing the spring and damping characteristics of the proposed ERSU, equivalent 2 DOF 1/12 tracked vehicle model is then formulated by regarding the spring and viscous damping coefficients under the static state as constant values. A robust LSDP(loop-shaping design procedure) $H_{\infty}$ controller compensating spring and damping parameter variations is then designed in order to suppress unwanted vibration of the vehicle. The control responses such as vertical and pitch acceleration are presented in time domain.

• 대한기계학회논문집A
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• 제37권6호
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• pp.805-814
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• 2013

유압식 Dipod 플랫폼은 기동차량에서 위성을 지향하는 안테나의 안정화 및 추적에 사용된다. 이러한 플랜트의 제어기 설계에는 외란제거와 추적 두 가지 성능목표 뿐만 아니라 강인성을 함께 절충해야 하는 제약조건으로 인해 1자유도 제어기에 비해 설계 유연성이 큰 2자유도 $H_{\infty}$ 제어기가 선호된다. $H_{\infty}$ 기반한 2자유도 제어기 종합방법에는 두 가지 프레임웍이 사용되는데 유압식 Dipod 플랫폼의 예를 통해서 일괄종합 방법이 더 우수한 성능을 보인 반면 분리종합 방법은 더 우수한 강인성을 보임을 확인할 수 있었다. $H_{\infty}$ 2자유도 종합방법에 따른 이러한 두 결과의 차이를 시스템 정합행렬의 구조화 특성을 통해 비교하여 보았다.