Hybrid spacecraft attitude control system
The hybrid subsystem design could be an attractive approach for futurespacecraft to cope with their demands. The idea of combining theconventional Attitude Control System and the Electrical Power System ispresented in this article. The Combined Energy and Attitude ControlSystem (CEACS) consisting of...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Multi-Science Publishing
2016-02-01
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| Series: | International Journal of Multiphysics |
| Online Access: | http://journal.multiphysics.org/index.php/IJM/article/view/19 |