Nonsingular terminal sliding mode based finite-time control for spacecraft attitude tracking
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/s12555-013-0247-x.pdf
Reference31 articles.
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3. D. Yang, Z. Chen, and X. Liu, “Distributed adaptive attitude tracking of multiple spacecraft with a leader of nonzero input,” International Journal of Control, Automation, and Systems, vol. 11, no. 5, pp. 938–946, 2013.
4. J. Su and K. Cai, “Globally stabilizing proportional -integral-derivative control laws for rigid-body attitude tracking,” Journal of Guidance Control and Dynamics, vol. 34, no. 4, pp. 1260–1264, 2011.
5. O. Egeland and J. M. Godhavn, “Passivity-based adaptive control of a rigid spacecraft,” IEEE Trans. on Automatic Control, vol. 39, no. 4, pp. 842–845, 1994.
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