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A Second-Order Sliding Mode Controller Design for Spacecraft Tracking Control
Joint Authors
Source
Mathematical Problems in Engineering
Issue
Vol. 2013, Issue 2013 (31 Dec. 2013), pp.1-9, 9 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2013-09-18
Country of Publication
Egypt
No. of Pages
9
Main Subjects
Abstract EN
For spacecraft attitude tracking system, there exists the chattering phenomenon.
In this paper, the spacecraft motion is decomposed into three-channel subsystems, and a second-order sliding mode control is proposed.
This method has been proved to have good convergence and robustness.
Combined with the proposed sliding surface, the three-channel controllers are designed.
The control performance is confirmed by the simulation results, the approaching process is improved effectively, and a smooth transition is achieved without overshoot and buffeting.
American Psychological Association (APA)
Zhao, Yu-Xin& Wu, Tian& Li, Gang. 2013. A Second-Order Sliding Mode Controller Design for Spacecraft Tracking Control. Mathematical Problems in Engineering،Vol. 2013, no. 2013, pp.1-9.
https://search.emarefa.net/detail/BIM-1031890
Modern Language Association (MLA)
Zhao, Yu-Xin…[et al.]. A Second-Order Sliding Mode Controller Design for Spacecraft Tracking Control. Mathematical Problems in Engineering No. 2013 (2013), pp.1-9.
https://search.emarefa.net/detail/BIM-1031890
American Medical Association (AMA)
Zhao, Yu-Xin& Wu, Tian& Li, Gang. A Second-Order Sliding Mode Controller Design for Spacecraft Tracking Control. Mathematical Problems in Engineering. 2013. Vol. 2013, no. 2013, pp.1-9.
https://search.emarefa.net/detail/BIM-1031890
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1031890