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Floquet-based design and control approach to spacecraft formation flying in libration point orbits 被引量:1

Floquet-based design and control approach to spacecraft formation flying in libration point orbits
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摘要 A method for spacecraft formation flying (SFF) design and control near libration point orbits was developed by making use of the Floquet theory for periodic orbits. Firstly, the Floquet theory used in libration point orbits was introduced and the coefficients of four Floquet periodic modes were proved to be nearly constant when the amplitude in z direction of earth-moon L1 halo orbits is less than 20000 km. On this basis, a configuration design approach to SFF in L1 halo orbits was proposed, and several types of special configurations were obtained with periodic mode 3 and mode 5 or mode 4 and mode 6. Then, in order to control the SFF configuration concisely, those coefficients of the 5 modes (except the stable one) must be kept constant. A stationkeeping method for SFF was developed, which controls 5 Floquet modes simultaneously. Finally, simulations showed that the Floquet-based approach of configuration design and control for SFF is effective, simple and convenient. The research may be of value for deep space explorations. A method for spacecraft formation flying (SFF) design and control near libration point orbits was developed by making use of the Floquet theory for periodic orbits. Firstly, the Floquet theory used in libration point orbits was introduced and the coefficients of four Floquet periodic modes were proved to be nearly constant when the amplitude in z direction of earth-moon L1 halo orbits is less than 20000 km. On this basis, a configuration design approach to SFF in L1 halo orbits was proposed, and several types of special configurations were obtained with periodic mode 3 and mode 5 or mode 4 and mode 6. Then, in order to control the SFF configuration concisely, those coefficients of the 5 modes (except the stable one) must be kept constant. A stationkeeping method for SFF was developed, which controls 5 Floquet modes simultaneously. Finally, simulations showed that the Floquet-based approach of configuration design and control for SFF is effective, simple and convenient. The research may be of value for deep space explorations.
出处 《Science China(Technological Sciences)》 SCIE EI CAS 2011年第3期758-766,共9页 中国科学(技术科学英文版)
基金 supported by the National Natural Science Foundation of China (Grant No. 10702078) the National University of Defense Technology Research Program (Grant No. JC08-01-05)
关键词 航天器飞行 轨道控制 飞行轨道 设计方法 平动点 基础 FLOQUET理论 周期模式 circular restricted three body problem spacecraft formation flying Floquet modes configuration design formation control
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参考文献20

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共引文献9

同被引文献13

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