제어로봇시스템학회:학술대회논문집
- 제어로봇시스템학회 1994년도 Proceedings of the Korea Automatic Control Conference, 9th (KACC) ; Taejeon, Korea; 17-20 Oct. 1994
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- Pages.232-237
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- 1994
An extended study of a spacecraft attitude and orbit control with an insufficient number of thrusters
- Imado, Fumiaki (Department of Mechanical Systems Engineering, Shinshu University) ;
- Ichikawa, Akira (Central Research Laboratory, Mitsubishi Electric Corporation)
- 발행 : 1994.10.01
초록
An extended study of optimal thruster combination for simultaneous attitude and orbital maneuvers of a jet-controled spacecraft is conducted. In this case, the spacecraft has not enough number of thrusters to control the rotation and translation separately. Therefore, thrusters are employed by combining to eliminate their coupling effects. The combinations are determined to minimize the fuel consumption. The redundancy study for some thruster failure cases is also presented.
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