TY - GEN
T1 - Back-stepping based integrated orbit and attitude control for on-orbit servicing spacecraft
AU - Lv, Yueyong
AU - Wang, Ziwei
AU - Guo, Yanning
AU - Chen, Liangming
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2017/1/20
Y1 - 2017/1/20
N2 - This paper investigates the integrated orbit and attitude modelling and control problem for on-orbit servicing spacecraft. The integrated relative kinematic and dynamic model for the on-orbit servicing spacecraft and the target is established on the base of dual-quaternion. A backstepping control law is proposed, which is improved then in consideration of system uncertainties. Globally asymptotical stability is analyzed through Lyapunov stability for the closed-loop system. Numerical simulations demonstrate the effectiveness and validity of the proposed methods.
AB - This paper investigates the integrated orbit and attitude modelling and control problem for on-orbit servicing spacecraft. The integrated relative kinematic and dynamic model for the on-orbit servicing spacecraft and the target is established on the base of dual-quaternion. A backstepping control law is proposed, which is improved then in consideration of system uncertainties. Globally asymptotical stability is analyzed through Lyapunov stability for the closed-loop system. Numerical simulations demonstrate the effectiveness and validity of the proposed methods.
UR - https://www.scopus.com/pages/publications/85015220732
U2 - 10.1109/CGNCC.2016.7829154
DO - 10.1109/CGNCC.2016.7829154
M3 - 会议稿件
AN - SCOPUS:85015220732
T3 - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
SP - 2325
EP - 2330
BT - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016
Y2 - 12 August 2016 through 14 August 2016
ER -