Autonomous multi satellites assembly in keplerian orbits
In this paper, the guidance and control algorithms of an autonomous multiple satellite assembly are developed in a general keplerian orbit. The guidance algorithms are based on defining the velocity profile of each satellite in two different segment of space. In the first segment, the guidance law u...
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| Main Authors: | , , |
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| Format: | Conference or Workshop Item |
| Language: | English |
| Published: |
American Institute of Aeronautics and Astronautics
2013
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/38417/1/Autonomous_Multi_Satellites_Assembly_in_Keplerian_Orbits.pdf http://irep.iium.edu.my/38417/ http://arc.aiaa.org/doi/abs/10.2514/6.2013-5195 |
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