Flywheel simultaneous attitude control and energy storage using a VSCMG configuration
Space vehicle programs consistently endeavor to reduce satellite bus mass to increase payload capacity and/or reduce launch and fabrication costs. At the same time, performance demands on satellite systems continue to increase, creating a formidable challenge to space vehicle technology development....
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Published in | 2000 IEEE International Conference on Control Applications pp. 991 - 995 |
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Main Authors | , |
Format | Conference Proceeding |
Language | English |
Published |
IEEE
2000
|
Subjects | |
Online Access | Get full text |
ISBN | 9780780365629 0780365623 |
DOI | 10.1109/CCA.2000.897602 |
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