首页|Force-position collaborative optimization of rope-driven snake manipulator for capturing non-cooperative space targets

Force-position collaborative optimization of rope-driven snake manipulator for capturing non-cooperative space targets

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With the rapid development of space activities,non-cooperative space targets increase swiftly,such as failed satellites and upper stages,threating normal spacecrafts seriously.As there are some problems in the capture process,such as excessive collision and fast tumbling of targets,manipulator with redundant Degrees of Freedom(DOFs)can be used to improve the compliance and therefore solve these problems.The Rope-Driven Snake Manipulator(RDSM)is a combina-tion of hyper-redundant DOFs and better compliance,and therefore it is suitable for capturing mis-sion.In this paper,a snake manipulator mechanism is designed,and the complete kinematic model and system dynamic model considering RDSM,target and contact is established.Then,to obtain the configuration of joint with hyper-redundant DOFs,an improved motion dexterity index is pro-posed as the joint motion optimization target.Besides,the force-position collaborative optimization index is designed to adjust active stiffness,and the impedance control method based on the modified index is used to capture the space target.Finally,the proposed force-position collaborative opti-mization method is verified by virtual prototype co-simulation.The results demonstrate that based on the proposed method,the collision force is reduced by about 25％compared to normal impe-dance control,showing higher safety.

Capturing non-cooperative space targetsRope-driven snake manipu-latorForce-position collaborative optimizationRedundant degrees of free-domActive stiffness adjustment

Xiaofeng LI、Jian TIAN、Cheng WEI、Xibin CAO

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School of Astronautics,Harbin Institute of Technology,Harbin 150001,China

Beijing Institute of Spacecraft System Engineering,China Academy of Space Technology,Beijing 100094,China

Science and Technology Department of Heilongjiang Province,ChinaNational Defense Key Laboratory of Space Intelligent Control Technology,China

JJ2022LH0315HTKJ2022KL502003

2024

10.1016/j.cja.2024.05.025

中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子：0.847
ISSN：1000-9361
年,卷(期)：2024.37(9)