NSSC OpenIR  > 空间技术部
Alternative TitleTransfer Trajectory Design for Halo Orbit with Multiple Constraints
李明涛; 郑建华; 于锡峥; 高东; 北京8701信箱
Source Publication宇航学报
KeywordHalo轨道 转移轨道 约束条件 微分修正
Other AbstractThere always exist constraints on transfer trajectory of libration point missions; however, p revious studies mainly focused on transfer trajectory design strategywithout constraints. This paper studied transfer trajectory design strategy for halo orbit with multip le constraints. Firstly, Constraints on transfer trajectory of libration point missions were analyzed. Then a generalmethod of transfer trajectory design with multip le constraintswas proposed, emphasiswas on the conclusion of differential corrections equations with the altitude, flight path angle, inclination and ascending node constraints.Finally, a halo orbit around the libration pointL1 of the Earth2Sun System was taken as the objective orbit, transfer trajectory with multip le constraintswas designed with the proposed method; simulation results validate the effectiveness of the proposed method.
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. 约束条件下的Halo轨道转移轨道设计[J]. 宇航学报,2009,30(2):437-441,509.
APA 李明涛,郑建华,于锡峥,高东,&北京8701信箱.(2009).约束条件下的Halo轨道转移轨道设计.宇航学报,30(2),437-441,509.
MLA 李明涛,et al."约束条件下的Halo轨道转移轨道设计".宇航学报 30.2(2009):437-441,509.
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