TY - JOUR
T1 - Trajectory Planning of Free-Floating Space Robot Based on Dual-Mode Switching
AU - Zhu, Zhanxia
AU - Wu, Tianyi
AU - Zhang, Guanghui
AU - Yu, Sigang
AU - Wang, Mingming
AU - Yuan, Jianping
N1 - Publisher Copyright:
© 2022 American Society of Civil Engineers.
PY - 2022/5/1
Y1 - 2022/5/1
N2 - For trajectory planning problem with multiconstraints of free-floating space robots (FFSR), the optimal solution may be unavailable due to strict constraints. In order to avoid identify a solution and obtain an executable joint trajectory, this paper proposes a trajectory planning method based on dual-mode switching. Using this method, the planner can automatically switch between the optimal mode and the effective mode, and obtain a feasible joint trajectory that satisfies the task requirements when the end-effector tracking error constraint and the joint torque constraint are considered. In this paper, the multiconstraints model of FFSR, which mainly consider control and dynamic constraints and the trajectory planning model based on dual-mode switching, are established, and the corresponding solving method is presented. The simulation results demonstrate that the proposed method is effective and feasible.
AB - For trajectory planning problem with multiconstraints of free-floating space robots (FFSR), the optimal solution may be unavailable due to strict constraints. In order to avoid identify a solution and obtain an executable joint trajectory, this paper proposes a trajectory planning method based on dual-mode switching. Using this method, the planner can automatically switch between the optimal mode and the effective mode, and obtain a feasible joint trajectory that satisfies the task requirements when the end-effector tracking error constraint and the joint torque constraint are considered. In this paper, the multiconstraints model of FFSR, which mainly consider control and dynamic constraints and the trajectory planning model based on dual-mode switching, are established, and the corresponding solving method is presented. The simulation results demonstrate that the proposed method is effective and feasible.
UR - http://www.scopus.com/inward/record.url?scp=85125648232&partnerID=8YFLogxK
U2 - 10.1061/(ASCE)AS.1943-5525.0001389
DO - 10.1061/(ASCE)AS.1943-5525.0001389
M3 - 文章
AN - SCOPUS:85125648232
SN - 0893-1321
VL - 35
JO - Journal of Aerospace Engineering
JF - Journal of Aerospace Engineering
IS - 3
M1 - 04022019
ER -