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ASME Press Select Proceedings

International Conference on Information Technology and Computer Science, 3rd (ITCS 2011)

Editor
V. E. Muhin
V. E. Muhin
National Technical University of Ukraine
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W. B. Hu
W. B. Hu
Wuhan University
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ISBN:
9780791859742
No. of Pages:
656
Publisher:
ASME Press
Publication date:
2011

In order to solve the problem of formation reconfiguration that is caused by the mission change or members in-out in the formation flying process, a multi-impulse control method was introduced to the reconfiguration for two special formations. The simulation result shows that the method was effective to formation in which the reference satellite was in the origin of the relative motion frame.

Abstract
Keywords
Introduction
Formation Foundation
Control Strategy for Formation Reconfiguration
Simulation Experiment
Conclusion
References
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