Robust H[infinity] control of spacecraft rendezvous on elliptical orbit
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Authors
Gao, X.
Teo, Kok Lay
Duan, G.
Date
2012Type
Journal Article
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Gao, X. and Teo, K.L. and Duan, G. 2012. Robust H[infinity] control of spacecraft rendezvous on elliptical orbit. Journal of the Franklin Institute. 349 (8): pp. 2515-2529.
Source Title
Journal of the Franklin Institute
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Department of Mathematics and Statistics
Collection
Abstract
This paper investigates the robust H∞H∞ control problem of spacecraft rendezvous on elliptical orbit. Based on Lyapunov theory, a sufficient condition for the existence of the robust H∞H∞ controller is given in terms of the periodic Riccati differential equation (RDE). Then, a stabilizable controller design method based on a fast multi-shot algorithm is proposed. With the controller obtained, the spacecraft rendezvous mission can be accomplished. An illustrative example is provided to show the effectiveness of the proposed control design method.
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