[1]LI Peng,CHEN Xing-lin,SONG Shen-min,et al.Research on an attitude and orbit coupling control over the final approach phase of rendezvous and docking[J].CAAI Transactions on Intelligent Systems,2010,5(6):530-533.
Copy

Research on an attitude and orbit coupling control over the final approach phase of rendezvous and docking

References:
[1]WALLSGROVE R J, AKELLA M R. Globally stabilizing saturated attitude control in the presence of bounded unknown disturbances[J]. Journal of Guidance Control and Dynamics, 2005, 28(5): 957963.
[2]Di GENNARO S. Stabilization of rigid spacecraft with uncertainties and input saturation in a central gravitational field[C]//Proceedings of 36th Conference on Decision and Control. San Diego, America, 1997: 42044209.
[3]VADALI S R. Variablestructure control of spacecraft largeangle maneuvers[J]. Journal of Guidance, Control and Dynamics, 1986, 9(2): 235239.
[4]DWYER T A W, SIRARAMIREZ H. Variable structure control of spacecraft attitude maneuvers[J]. Journal of Guidance, Control and Dynamics, 1988, 11(3): 262270.
[5]PUKDEBOON C, ZINOBER A S I, THEIN M W L. Quasicontinuous higherorder sliding mode controller designs for spacecraft attitude tracking manoeuvres[J]. 1998(1):22442250.
[6]FRIDMAN L, DAVILA J, LEVANT A. Highorder slidingmode observation and fault detection[C]//Proceedings of the 46th IEEE Conference on Decision and Control. New Orleans, USA, 2007: 437442.
[7]DOREL L,LEVANT A. On chatteringfree slidingmode control[C]//Proceedings of the 47th IEEE Conference on Decision and Control Cancun, Mexico, 2008: 11471156.
[8]LEVANT A. Principles of 2sliding mode design[J]. Automatic, 2007(43): 576586.
Similar References:

Memo

-

Last Update: 2011-03-03

Copyright © CAAI Transactions on Intelligent Systems