Journal of the Korea Institute of Military Science and Technology (한국군사과학기술학회지)
- Volume 4 Issue 2
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- Pages.147-156
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- 2001
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- 1598-9127(pISSN)
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- 2636-0640(eISSN)
A Robust Attitude Control Scheme Based on Eigenaxis Rotation for Spacecraft
고유축 회전에 근거한 우주비행체 강인 자세제어 기법
Abstract
In this paper, a robust attitude control scheme based on Eigenaxis rotation for the spacecraft is proposed. Eigenaxis rotation transforms the attitude of spacecraft to the shortest path and is represented by quaternion. The control law consists of PD-type control part for the nominal system and the robust control part for compensating inertia uncertainty. For the proposed controller, stability analysis is performed and the performance is shown via computer simulation.