TY - GEN
T1 - Orbital and attitude cooperative control of fly-around small satellite
AU - Zhu, Zhan Xia
AU - Yang, Jia
PY - 2008
Y1 - 2008
N2 - This paper deals with the problem of controlling both orbital and attitude states for a fly-around small satellite during proximity operations. Firstly, We derive the six degree of freedom error dynamics model. Then, for the uncertainties such as mass and inertia moment, we put forward an adaptive output feedback control method that can be used to solve above control problem and design the control law when considering translational and attitude coupling. Finally, the simulation results show that the designed control law is effective and the control method is feasible.
AB - This paper deals with the problem of controlling both orbital and attitude states for a fly-around small satellite during proximity operations. Firstly, We derive the six degree of freedom error dynamics model. Then, for the uncertainties such as mass and inertia moment, we put forward an adaptive output feedback control method that can be used to solve above control problem and design the control law when considering translational and attitude coupling. Finally, the simulation results show that the designed control law is effective and the control method is feasible.
UR - http://www.scopus.com/inward/record.url?scp=52449085225&partnerID=8YFLogxK
U2 - 10.1109/ICICIC.2008.411
DO - 10.1109/ICICIC.2008.411
M3 - 会议稿件
AN - SCOPUS:52449085225
SN - 9780769531618
T3 - 3rd International Conference on Innovative Computing Information and Control, ICICIC'08
BT - 3rd International Conference on Innovative Computing Information and Control, ICICIC'08
T2 - 3rd International Conference on Innovative Computing Information and Control, ICICIC'08
Y2 - 18 June 2008 through 20 June 2008
ER -