Robust control for spacecraft rendezvous with disturbances and input saturation
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/s12555-013-0530-x.pdf
Reference18 articles.
1. P. Singla, K. Subbarao, and J. Junkins, “Adaptive output feedback control for spacecraft rendezvous and docking under measurement uncertainty,” Journal of Guidance, Control, and Dynamics, vol. 29, no. 4, pp. 892–902, July 2006.
2. C. D. Karlgaard, “Robust rendezvous navigation in elliptical orbit,” Journal of Guidance, Control, and Dynamics, vol. 29, no. 2, pp. 495–499, March 2006.
3. B. Ebrahimi, M. Bahrami, and J. Roshanian, “Optimal sliding-mode guidance with terminal velocity constraint for fixed-interval propulsive maneuvers,” Acta Astronautica, vol. 62, no. 10, pp. 556–562, May 2008.
4. B. Zhou, Z. Lin, and G. R. Duan, “Lyapunov differential equation approach to elliptical orbital rendezvous with constrained controls,” Journal of Guidance, Control, and Dynamics, vol. 34, no. 2, pp. 345–358, March 2011.
5. L. C. Ma, X. Y. Meng, Z. Z. Liu, and L. F. Du, “Suboptimal power-limited rendezvous with fixed docking direction and collision avoidance,” Journal of Guidance, Control, and Dynamics, vol. 36, no. 1, pp. 229–239, January 2013.
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