제어로봇시스템학회:학술대회논문집
- 제어로봇시스템학회 1994년도 Proceedings of the Korea Automatic Control Conference, 9th (KACC) ; Taejeon, Korea; 17-20 Oct. 1994
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- Pages.44-48
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- 1994
Large slewing control of low earth orbit satellite
- Rhee, S.W. (Senior Member of Research Staff, TT&C Section, Satellite Communications R&D Division, ETRI, Yusong P.O.Box 106, Taejon, 305-600)
- 발행 : 1994.10.01
초록
A new method of quaternion feedback control for the attitude acquisition of spacecraft is suggested to limit the angular rates of rigid body which are not desirable and make a control algorithm complicate. New attitude acquisition control algorithm is evaluated and compared with the existing quaternion feedback control method for the large slewing maneuvers through simulations. The simulation results reveal that a new method is effective on limiting the angular rates of spacecraft.
키워드