Adaptive output feedback integral sliding mode attitude tracking control of spacecraft without unwinding
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Title
Adaptive output feedback integral sliding mode attitude tracking control of spacecraft without unwinding
Authors
Keywords
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Journal
Advances in Mechanical Engineering
Volume 9, Issue 7, Pages 168781401771040
Publisher
SAGE Publications
Online
2017-07-21
DOI
10.1177/1687814017710406
References
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Related references
Note: Only part of the references are listed.- Smooth finite-time fault-tolerant attitude tracking control for rigid spacecraft
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- Adaptive fuzzy fault-tolerant attitude control of spacecraft
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- (2010) F.-K. Yeh IET Control Theory and Applications
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- (2009) Zhiyong Chen et al. IEEE TRANSACTIONS ON AUTOMATIC CONTROL
- Quasi-Continuous Higher Order Sliding-Mode Controllers for Spacecraft-Attitude-Tracking Maneuvers
- (2009) C. Pukdeboon et al. IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS
- Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control
- (2007) Erdong Jin et al. AEROSPACE SCIENCE AND TECHNOLOGY
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