TY - JOUR
T1 - Capture and detumble of a non-cooperative target without a specific gripping point by a dual-arm space robot
AU - Han, Dong
AU - Liu, Zhengxiong
AU - Huang, Panfeng
N1 - Publisher Copyright:
© 2022 COSPAR
PY - 2022/5/15
Y1 - 2022/5/15
N2 - This paper focuses on the control strategy of a dual-arm space robot to capture and detumble a non-cooperative satellite without a specific gripping point. First, an elastic hemispherical claw was designed to reduce the collision impacts and adjust the capture position, and its contact dynamics and capture ability were verified by ground experiments. Analysis of the position constraints led to the proposal of a compliant control scheme to achieve stable capture without a contact-force sensor. Subsequently, a modified adaptive sliding mode based prescribed trajectory tracking control (PTTC) and null space intersection approach was proposed to achieve target detumbling under the actuator constraints. The control system stability was analyzed via the Lyapunov method. Finally, numerical simulations were employed to validate the effectiveness and correctness of the strategy. Results showed that, a large inertia target could be steadily captured and detumbled within 80 s.
AB - This paper focuses on the control strategy of a dual-arm space robot to capture and detumble a non-cooperative satellite without a specific gripping point. First, an elastic hemispherical claw was designed to reduce the collision impacts and adjust the capture position, and its contact dynamics and capture ability were verified by ground experiments. Analysis of the position constraints led to the proposal of a compliant control scheme to achieve stable capture without a contact-force sensor. Subsequently, a modified adaptive sliding mode based prescribed trajectory tracking control (PTTC) and null space intersection approach was proposed to achieve target detumbling under the actuator constraints. The control system stability was analyzed via the Lyapunov method. Finally, numerical simulations were employed to validate the effectiveness and correctness of the strategy. Results showed that, a large inertia target could be steadily captured and detumbled within 80 s.
KW - Active debris removal
KW - Compliant control
KW - Dual-arm space robot
KW - Prescribed trajectory tracking control
UR - http://www.scopus.com/inward/record.url?scp=85126577997&partnerID=8YFLogxK
U2 - 10.1016/j.asr.2022.02.039
DO - 10.1016/j.asr.2022.02.039
M3 - 文章
AN - SCOPUS:85126577997
SN - 0273-1177
VL - 69
SP - 3770
EP - 3784
JO - Advances in Space Research
JF - Advances in Space Research
IS - 10
ER -