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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| Pengarang-pengarang Utama: | , |
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| Format: | Artikel |
| Bahasa: | English English |
| Diterbitkan: |
Instituto de Aeronautica e Espaco-IAE - Brazil
2014
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| Subjek-subjek: | |
| Capaian Atas Talian: | http://irep.iium.edu.my/38405/ http://irep.iium.edu.my/38405/ http://irep.iium.edu.my/38405/ http://irep.iium.edu.my/38405/1/38405_Relative%20motion%20guidance%2C%20navigation.pdf http://irep.iium.edu.my/38405/2/38405_Relative%20motion%20guidance%2C%20navigation_SCOPUS.pdf |
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