NSSC OpenIR  > 空间技术部
Alternative TitleAutomated Design and Simulation of Gravity-Assist Trajectories for Deep Space Probe
李志武; 郑建华; 于锡峥; 吴霞; 北京8701信箱
Source Publication计算机仿真
Keyword借力飞行 多天体交会 轨道设计 仿真
Other AbstractAs the direct transfer trajectories needmore energy in deep space exp loration, gravity-assist trajectories can reduce launch energy from the earth,and enable the p robe to exp lore more celestial bodies in one mission.Trajectorieswhich may exist can be speculated out by drawing P-Rp graphics,then launch windowswould be found by solving Lambertps p roblem and drawing energy contour figures. Two programs are developed to design trajectories and search windows. The analysismethod, the correctness and reliability of the sofeware are validated by EVEEJ project and its simulation in STK. This paper brings out integrated design technology for gravity-assist trajectories, and provides reference for deep space exp loration.
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
李志武,郑建华,于锡峥,等. 深空探测行星借力飞行轨道自动设计与仿真[J]. 计算机仿真,2009,26(6):59-61,73.
APA 李志武,郑建华,于锡峥,吴霞,&北京8701信箱.(2009).深空探测行星借力飞行轨道自动设计与仿真.计算机仿真,26(6),59-61,73.
MLA 李志武,et al."深空探测行星借力飞行轨道自动设计与仿真".计算机仿真 26.6(2009):59-61,73.
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