TY - JOUR
T1 - Robust control of a dual-arm space robot for in-orbit screw-driving operation
AU - Wang, Xiaoyi
AU - Shi, Lingling
AU - Katupitiya, Jayantha
N1 - Publisher Copyright:
© 2022 IAA
PY - 2022/11
Y1 - 2022/11
N2 - As large-scale spacecraft like Hubble Space Telescope need in-orbit assembly, there is an increasing need for the in-orbit assembly automatically carried out by space robots. This paper proposes a potential in-orbit screw-driving strategy carried out by a dual-arm space robot. Unlike single-arm space robots, a dual-arm space robot can avoid the translation and rotation of the target during the screw-driving process. For explanation, one arm can be set as the mission arm in the screw-driving process. The other arm can simultaneously provide the opposite contact forces and torques applied to the target. The hybrid position/force control strategy is developed for a dual-arm space robot to precisely deliver the desired contact forces by the end-effectors. Moreover, the base attitude of the space robot is controlled by reaction wheels to reduce the coupled movement between the base and the manipulators. According to a typical screw-driving procedure for automatic assembly, a desired fastening torque–angle curve is designed to ensure that the screw is firmly tightened. A robust Sliding Mode Controller (SMC) is designed to perform well against the uncertainties and disturbances applied to the space robot system. The simulation results show the feasibility of the potential dual-arm in-orbit screw-driving strategy.
AB - As large-scale spacecraft like Hubble Space Telescope need in-orbit assembly, there is an increasing need for the in-orbit assembly automatically carried out by space robots. This paper proposes a potential in-orbit screw-driving strategy carried out by a dual-arm space robot. Unlike single-arm space robots, a dual-arm space robot can avoid the translation and rotation of the target during the screw-driving process. For explanation, one arm can be set as the mission arm in the screw-driving process. The other arm can simultaneously provide the opposite contact forces and torques applied to the target. The hybrid position/force control strategy is developed for a dual-arm space robot to precisely deliver the desired contact forces by the end-effectors. Moreover, the base attitude of the space robot is controlled by reaction wheels to reduce the coupled movement between the base and the manipulators. According to a typical screw-driving procedure for automatic assembly, a desired fastening torque–angle curve is designed to ensure that the screw is firmly tightened. A robust Sliding Mode Controller (SMC) is designed to perform well against the uncertainties and disturbances applied to the space robot system. The simulation results show the feasibility of the potential dual-arm in-orbit screw-driving strategy.
KW - Dual-arm space robot
KW - Hybrid position/force control
KW - In-orbit assembly
KW - Screw-driving process
KW - Sliding mode control
UR - http://www.scopus.com/inward/record.url?scp=85136174137&partnerID=8YFLogxK
U2 - 10.1016/j.actaastro.2022.07.048
DO - 10.1016/j.actaastro.2022.07.048
M3 - Article
AN - SCOPUS:85136174137
SN - 0094-5765
VL - 200
SP - 139
EP - 148
JO - Acta Astronautica
JF - Acta Astronautica
ER -