TY - GEN
T1 - Hybrid control strategy for attitude stabilization of an underactuated spacecraft with two moving mass
AU - Jiang, Yu
AU - He, Fenghua
AU - Yao, Yu
PY - 2007
Y1 - 2007
N2 - Motivated by the attitude control of an under-actuated spacecraft with two moving mass, we consider the stabilization problem of nonlinear systems via hybrid control strategy. First, the spacecraft is modeled based on principle of conservation of momentum and characteristic of model is analyzed. Hybrid control architecture for attitude system is described and feedback controllers are constructed by switching between several feedback functions which are selected to accomplish a sequence of spacecraft maneuvers.
AB - Motivated by the attitude control of an under-actuated spacecraft with two moving mass, we consider the stabilization problem of nonlinear systems via hybrid control strategy. First, the spacecraft is modeled based on principle of conservation of momentum and characteristic of model is analyzed. Hybrid control architecture for attitude system is described and feedback controllers are constructed by switching between several feedback functions which are selected to accomplish a sequence of spacecraft maneuvers.
KW - Attitude stabilization
KW - Hybrid control strategy
KW - Under-actuated spacecraft
UR - https://www.scopus.com/pages/publications/40649104175
U2 - 10.1109/ICAL.2007.4338593
DO - 10.1109/ICAL.2007.4338593
M3 - 会议稿件
AN - SCOPUS:40649104175
SN - 1424415314
SN - 9781424415311
T3 - Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2007
SP - 389
EP - 393
BT - Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2007
T2 - 2007 IEEE International Conference on Automation and Logistics, ICAL 2007
Y2 - 18 August 2007 through 21 August 2007
ER -