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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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Bibliographic Details
Published in:Journal of guidance, control, and dynamics control, and dynamics, 2009-01, Vol.32 (1), p.290-299
Main Authors: Hamel, Jean-Francois, Lafontaine, Jean De
Format: Article
Language:English
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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]
ISSN:0731-5090
1533-3884
DOI:10.2514/1.32778