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https://hdl.handle.net/2440/87499
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Type: | Journal article |
Title: | Multi-objective robust H∞ control of spacecraft rendezvous |
Other Titles: | Multi-objective robust H-infinity control of spacecraft rendezvous |
Author: | Gao, H. Yang, X. Shi, P. |
Citation: | IEEE Transactions on Control Systems Technology, 2009; 17(4):794-802 |
Publisher: | Institute of Electrical and Electronics Engineers |
Issue Date: | 2009 |
ISSN: | 1063-6536 1558-0865 |
Statement of Responsibility: | Huijun Gao, Xuebo Yang, and Peng Shi |
Abstract: | Based on the relative motion dynamic model illustrated by C-W equations, the problem of robust Hinfin control for a class of spacecraft rendezvous systems is investigated, which contains parametric uncertainties, external disturbances and input constraints. An Hinfin state-feedback controller is designed via a Lyapunov approach, which guarantees the closed-loop system to meet the multi-objective design requirements. The existence conditions for admissible controllers are formulated in the form of linear matrix inequalities (LMIs), and the controller design is cast into a convex optimization problem subject to LMI constraints. An illustrative example is provided to show the effectiveness of the proposed control design method. |
Keywords: | C-W equations H-infinity control input constraint linear matrix inequalities (LMIs) rendezvous uncertainty |
Rights: | © 2009 IEEE |
DOI: | 10.1109/TCST.2008.2012166 |
Published version: | http://dx.doi.org/10.1109/tcst.2008.2012166 |
Appears in Collections: | Aurora harvest 7 Electrical and Electronic Engineering publications |
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