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Pacific-Asia Workshop on Computational Intelligence and Industrial Application, IEEE (2008)
Dec. 19, 2008 to Dec. 20, 2008
ISBN: 978-0-7695-3490-9
pp: 149-153
ABSTRACT
The problem of stabilization was studied for an underactuated rigid spacecraft. First of all, the system dynamic and kinematic equations are given, the kinematic equation is described by the (w, z) parametrization. Some continuous time-varying control laws are then designed based on the characteristic of the system model. The accessorial variables and
INDEX TERMS
Underactuated system, Attitude stabilization, Backstepping control, Time-varying control
CITATION
Yanqin Zheng, Xinsheng Ge, "A Time-Varying Control of an Underactuated Rigid Spacecraft", Pacific-Asia Workshop on Computational Intelligence and Industrial Application, IEEE, vol. 01, no. , pp. 149-153, 2008, doi:10.1109/PACIIA.2008.80
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