Modeling, dynamics and control of spacecraft relative motion in a perturbed keplerian orbit
The dynamics of relative motion in a perturbed orbital environment are exploited based on Gauss’ and Cowell’s variational equations. The inertial coordinate frame and relative coordinate frame (Hill frame) are used, and a linear high fidelity model is developed to describe the relative motion. This...
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| Main Authors: | , |
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| Format: | Article |
| Language: | English English |
| Published: |
The Korean Society for Aeronautical & Space Sciences
2015
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/42772/1/8%2877-88%2914-064.pdf http://irep.iium.edu.my/42772/4/42772-_wos%2Cscopus.pdf http://irep.iium.edu.my/42772/ http://ijass.org/On_line/admin/files/8(77~88)14-064.pdf http://dx.doi.org/10.5139/IJASS.2015.16.1.77 |
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