Title :
Attitude control of a tethered spacecraft
Author :
Cho, Sangbum ; McClamroch, N. Harris
Author_Institution :
University of Michigan
Keywords :
Actuators; Aerodynamics; Attitude control; Force control; Linear feedback control systems; Mathematical model; Motion analysis; Motion control; Nonlinear equations; Space vehicles;
Conference_Titel :
American Control Conference, 2003. Proceedings of the 2003
Print_ISBN :
0-7803-7896-2
DOI :
10.1109/ACC.2003.1239734