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Chen Ying Chen Zugui Liu Liangdong (Beijing Institute of Control Engineering,Beijing 100080)
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Abstract: The problem of optimal bounded thrust time fixed rendezvous of two spacecraft is investigated in this paper.Several properties on optimal thrust arcs are presented on the basis of the rendezvous process of spacecraft.These results have provided the theoretical fundamentals for the engineering design of rendezvous and docking of spacecraft.
Chen Ying Chen Zugui Liu Liangdong (Beijing Institute of Control Engineering,Beijing 100080). OPTIMAL BOUNDED THRUST TIME FIXED RENDEZVOUS OF SPACECRAFT[J]. .
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