| Halo轨道编队构型重构最优控制研究 |
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| 引用本文： | 张跃东,孟云鹤,桂忱,戴金海.Halo轨道编队构型重构最优控制研究[J].国防科技大学学报,2011,33(4):24-29. |
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| 作者姓名： | 张跃东 孟云鹤 桂忱 戴金海 |
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| 作者单位： | 1. 国防科技大学航天与材料工程学院,湖南长沙,410073
2. 长沙理工大学,湖南长沙,410004 |
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| 基金项目： | 国家自然科学基金资助项目(10702078); 国防科技大学预研基金资助项目(JC08-01-05) |
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| 摘 要： | 变长度的测量基线与空间构型的多样性是航天器以编队方式执行深空探测任务的优势之一,该优势的发挥与航天器编队构型重构能力密切相关.针对Halo轨道编队构型重构问题开展研究,分析了Halo轨道编队的构型特性,推导了Halo轨道编队构型重构最优控制的Hamilton方程,基于第一类生成函数构造了最优控制Hamilton方程的迭...
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| 关 键 词： | 平动点 Halo轨道编队 构型重构 最优控制 生成函数法 |
| 收稿时间： | 2010/12/3 0:00:00 |
Study on Optimal Control for Halo Orbits Formation Reconfiguration |
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| ZHANG Yuedong,Meng Yunhe,Gui Chen and DAI Jinhai.Study on Optimal Control for Halo Orbits Formation Reconfiguration[J].Journal of National University of Defense Technology,2011,33(4):24-29. |
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| Authors: | ZHANG Yuedong Meng Yunhe Gui Chen and DAI Jinhai |
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| Institution: | ZHANG Yue-dong1,Meng Yun-he1,Gui Chen2,DAI Jin-hai1(1.College of Aerospace and Material Engineering,National Univ.of Defense Technology,Changsha 410073,China,2.Changsha Univ.of Science and Technology,China) |
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| Abstract: | Changeable measurement baseline and diversity of space configuration are advantages of spacecraft formation implementing deep-space exploration mission.They are closely related to the reconfiguration capability of spacecraft formation.Aimed at the issue of optimal control for Halo orbits formation reconfiguration,this study firstly analyzed the configuration characteristics of Halo orbits formation,then the Hamiltonian equation of optimal control for Halo orbits formation reconfiguration were deduced.Iterat... |
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| Keywords: | libration points halo orbits formation formation reconfiguration optimal control generating function method |
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