Dynamic Modeling and LQG/LTR Controller Design for the Flexible Structures

유연 구조물에 대한 동역학 모델링 및 LQG/LTR 제어기 설계

  • Published : 2004.02.01

Abstract

Some of Spacecraft's structures are flexible so that a certain expected disturbance can easily excite a low frequency vibration on these structures, having very low natural damping. Such vibration will degrade the performance of the system, which should to be kept in a specific shape or attitude against the undesired vibration. In this paper, LQG/LTR controller is developed using an additional dynamic model to increase the performance of the frequency responses at low frequency area. This study presents that the LQG/LTR design was an effective controller for the flexible structure.

Keywords

References

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