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Neighboring Optimum Feedback Control Law for Earth-Orbiting Formation-Flying Spacecraft
This paper develops a feedback control law that guarantees neighboring fuel-optimality of the reconfiguration of a formation of Earth-orbiting formation-flying spacecraft. It aims for the case in which a specific formation is to be achieved at a specific true anomaly. It guarantees neighboring fuel-...
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Published in: | Journal of guidance, control, and dynamics control, and dynamics, 2009-01, Vol.32 (1), p.290-299 |
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Main Authors: | , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | This paper develops a feedback control law that guarantees neighboring fuel-optimality of the reconfiguration of a formation of Earth-orbiting formation-flying spacecraft. It aims for the case in which a specific formation is to be achieved at a specific true anomaly. It guarantees neighboring fuel-optimality of such a reconfiguration maneuver, assuming that the formation evolves in the vicinity of an uncontrolled reference trajectory. It is in the semi-analytic form, as only one time-varying gain matrix needs to be computed before the maneuver. It allows a fuel consumption/formation accuracy tradeoff with the selection of only one scalar gain. Simulations compare the performance of this controller with the linear-quadratic regulator and the mean orbit elements controller in the context of a 1 km size formation reconfiguration. Simulations show that this neighboring optimum controller can perform the maneuver with better accuracy while spending as much or less propellant than the other controllers. [PUBLISHER ABSTRACT] |
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ISSN: | 0731-5090 1533-3884 |
DOI: | 10.2514/1.32778 |