TY - GEN
T1 - Deep space explorer attitude maneuver planning based on sliding mode control
AU - Wu, Changqing
AU - Xu, Rui
AU - Zhu, Shengying
AU - Yang, Nan
AU - Wang, Lina
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2016/8/3
Y1 - 2016/8/3
N2 - During the deep space exploration missions a lot of attitude maneuvers need to be completed for the change of different attitude. Meanwhile, in the course of the explorer attitude maneuver there are many attitude pointing constraints due to the diversity of space tasks. Firstly, attitude kinematic and dynamic equations based on quaternion are established in this paper, which laid the foundation for design and simulation of the planning system. Secondly, to improve system stability and robustness of strong disturbance, an autonomous attitude planning system based sliding mode control has been proposed. In addition, a constraint monitor module ensures that the attitude commands received from the attitude controllers do not violate attitude pointing constraints. Finally, simulation results demonstrate that: the methods in this paper not only meet complex attitude pointing constraints but also achieve high-precision attitude maneuver in large angle maneuver under high time-varying disturbance torque, and the attitude maneuver path is smoother and feasible for implementation.
AB - During the deep space exploration missions a lot of attitude maneuvers need to be completed for the change of different attitude. Meanwhile, in the course of the explorer attitude maneuver there are many attitude pointing constraints due to the diversity of space tasks. Firstly, attitude kinematic and dynamic equations based on quaternion are established in this paper, which laid the foundation for design and simulation of the planning system. Secondly, to improve system stability and robustness of strong disturbance, an autonomous attitude planning system based sliding mode control has been proposed. In addition, a constraint monitor module ensures that the attitude commands received from the attitude controllers do not violate attitude pointing constraints. Finally, simulation results demonstrate that: the methods in this paper not only meet complex attitude pointing constraints but also achieve high-precision attitude maneuver in large angle maneuver under high time-varying disturbance torque, and the attitude maneuver path is smoother and feasible for implementation.
KW - Attitude maneuver
KW - Deep space exploration
KW - Path planning
KW - Sliding mode control
UR - http://www.scopus.com/inward/record.url?scp=84983755265&partnerID=8YFLogxK
U2 - 10.1109/CCDC.2016.7531067
DO - 10.1109/CCDC.2016.7531067
M3 - Conference contribution
AN - SCOPUS:84983755265
T3 - Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016
SP - 658
EP - 663
BT - Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 28th Chinese Control and Decision Conference, CCDC 2016
Y2 - 28 May 2016 through 30 May 2016
ER -