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...

詳細記述

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書誌詳細
主要な著者: Okasha, Mohamed Elsayed Aly Abd Elaziz, Newman, Brett
フォーマット: Conference or Workshop Item
言語:English
出版事項: 2011
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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