Dynamic surface active fault tolerant control design for the attitude control systems of UAV with actuator fault
Author:
Publisher
Springer Science and Business Media LLC
Subject
Computer Science Applications,Control and Systems Engineering
Link
http://link.springer.com/content/pdf/10.1007/s12555-015-0020-4.pdf
Reference28 articles.
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3. Z. F. Gao, J. X. Lin and T. Cao, “Robust fault tole-rant tracking control design for a linearized hyper-sonic vehicle with sensor fault,” International Journal of Control, Automation, and Systems, vol. 13, no. 3, pp. 672–679, 2015.
4. W. MacKunis, Z. D. Wilcox, M. K. Kaiser, and W. E. Dixon, “Global adaptive output feedback tracking control of an unmanned aerial vehicle,” IEEE Transactions on Control Systems Technology, vol. 18, no. 6, pp. 1390–1397, 2010. [click] Fig. 10. The fault tolerant control input dF in actuator faulty case.
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