Relative motion guidance, navigation and control for autonomous orbital rendezvous
In this paper, the dynamics of the relative motion problem in a perturbed orbital environment are exploited based on Gauss’ variational equations. The relative coordinate frame (Hill frame) is studied to describe the relative motion. A linear high fidelity model is developed to describe the relative...
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主要な著者: | , |
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フォーマット: | Conference or Workshop Item |
言語: | English |
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2011
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主題: | |
オンライン・アクセス: | http://irep.iium.edu.my/38705/1/6%252E2011-6427.pdf http://irep.iium.edu.my/38705/ http://arc.aiaa.org/doi/abs/10.2514/6.2011-6427 |
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