基于圆型限制性三体问题模型的行星卫星逃逸能量研究

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2007, Vol. 28 ›› Issue (2): 263-268.

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Study on Escaping Energy in Circular Restricted Three body Problem

HE Wei,XU Shi-jie

School of Astronautics, Beijing University of Aeronautics and Astronautics

Received:2005-10-26 Revised:2006-07-19 Online:2007-03-10 Published:2007-03-10
Contact: XU Shijie

Abstract

Abstract:

Escaping trajectories are investigated using a Poincaré map method in the circular restricted three body problem consisting of spacecraft, planet and moon. On the condition that Jacobi constant is fixed, the escaping trajectories are integrated back to the first periapsis from vicinity of L-1 and L-2 and the escaping velocity of moon is obtained.

Key words: escaping , trajectory, , circular , restricted , three , body , problem, , Poincaré, , section

CLC Number:

V412.4

HE Wei;XU Shi-jie. Study on Escaping Energy in Circular Restricted Three body Problem[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2007, 28(2): 263-268.

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Study on Escaping Energy in Circular Restricted Three body Problem

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