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Robust H∞ Control for Spacecraft Rendezvous with a Noncooperative Target
Joint Authors
Wu, Guo-Qiang
Wu, Shu-Nan
Tan, Shu-Jun
Zhou, Wenya
Source
Issue
Vol. 2013, Issue 2013 (31 Dec. 2013), pp.1-7, 7 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2013-08-20
Country of Publication
Egypt
No. of Pages
7
Main Subjects
Medicine
Information Technology and Computer Science
Abstract EN
The robust H∞ control for spacecraft rendezvous with a noncooperative target is addressed in this paper.
The relative motion of chaser and noncooperative target is firstly modeled as the uncertain system, which contains uncertain orbit parameter and mass.
Then the H∞ performance and finite time performance are proposed, and a robust H∞ controller is developed to drive the chaser to rendezvous with the non-cooperative target in the presence of control input saturation, measurement error, and thrust error.
The linear matrix inequality technology is used to derive the sufficient condition of the proposed controller.
An illustrative example is finally provided to demonstrate the effectiveness of the controller.
American Psychological Association (APA)
Wu, Shu-Nan& Zhou, Wenya& Tan, Shu-Jun& Wu, Guo-Qiang. 2013. Robust H∞ Control for Spacecraft Rendezvous with a Noncooperative Target. The Scientific World Journal،Vol. 2013, no. 2013, pp.1-7.
https://search.emarefa.net/detail/BIM-1033072
Modern Language Association (MLA)
Wu, Shu-Nan…[et al.]. Robust H∞ Control for Spacecraft Rendezvous with a Noncooperative Target. The Scientific World Journal No. 2013 (2013), pp.1-7.
https://search.emarefa.net/detail/BIM-1033072
American Medical Association (AMA)
Wu, Shu-Nan& Zhou, Wenya& Tan, Shu-Jun& Wu, Guo-Qiang. Robust H∞ Control for Spacecraft Rendezvous with a Noncooperative Target. The Scientific World Journal. 2013. Vol. 2013, no. 2013, pp.1-7.
https://search.emarefa.net/detail/BIM-1033072
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1033072