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He Yan (Beijing Institute of Systems Engineering,Beijing 100101) Tan Xichun (Institute of Command and Technology,Beijing 101416)
Published:
Abstract: This paper has analyzed all kinds of perturbation forces affecting spacecraft in space in detail,and got a precise model of orbit calculation of spacecraft,and has set up a precise model of relative movement between two spacecraft in space rendezvous and docking.With this error scaling criterion,this paper has analyzed the calculation error of Hill equation in the end.
He Yan (Beijing Institute of Systems Engineering,Beijing 100101) Tan Xichun (Institute of Command and Technology,Beijing 101416). RESEARCH OF CALCULATION ERROR PROPERTY OF HILL EQUATION IN SPACE RENDEZVOUS AND DOCKING[J]. .
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