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Alternative TitleResearch on the Perturbed Three-body Problem
李明涛; 郑建华; 于锡峥; 高东; 北京8701信箱
Source Publication中国空间科学技术
Keyword受摄三体问题 四体问题 椭圆限制性三体问题 动力学 深空探测
Other AbstractSince the circular rest ricted t hree-body problem model ignores t he effect of pert urbations , it can not accurately describe the dynamic characters of t he three2body system. The dynamic character s and orbit design st rategy of the pert urbed t hree2body problem model was studied. Fir stly , main pert urbations of libration point missions were analyzed , and t hen t he general dynamic equation of the perturbed three-body problem in the synodic f rame was concluded f rom t he dynamic equations in the inertial f rame considering the effect s of the eccent ricity , the gravity of t he fourt h body and the solar radiation pressure. Finally , t he two level differential corrections met hod was propo sed to t ransform t he orbit designed under the circular rest ricted t hree-body problem model into t he perturbed three2body problem model .
Indexed ByCSCD
Funding Project中国科学院空间科学与应用研究中心
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Document Type期刊论文
Corresponding Author北京8701信箱
Recommended Citation
GB/T 7714
李明涛,郑建华,于锡峥,等. 受摄三体问题研究[J]. 中国空间科学技术,2008,28(6):14-20.
APA 李明涛,郑建华,于锡峥,高东,&北京8701信箱.(2008).受摄三体问题研究.中国空间科学技术,28(6),14-20.
MLA 李明涛,et al."受摄三体问题研究".中国空间科学技术 28.6(2008):14-20.
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