Dynamic modeling and analysis of an in-space cable-driven manipulator for on-orbit servicing

• Kinematics of a cable-driven manipulator is analyzed and its motion planning scheme is designed. • Two dynamic models of the cable-driven manipulator are established and cross-verified. • Tension decay factor is applied to model the frictional contact in cable-pulley systems. • Simulations are performed to investigate the influences of structural parameters on manipulator dynamics. • Ground experiments are carried out to verify the kinematic and dynamic model. In-space cable-driven manipulators exhibit several advantages, such as a large range of motion, high dexterity, and lightweight structure. However, kinematic and dynamic analysis play an essential role in designing a cable-driven manipulator. In this paper, the kinematic analysis of a type of cable-driven manipulator is performed, and a motion planning scheme is conducted to actuate this manipulator. Moreover, a flexible multi-body dynamic model of a cable-driven manipulator considering the frictional contact between the cables and pulleys is established. To describe properties such as flexibility, vibration, and variable length of the cable, this paper utilizes reduced-order beam elements of the Absolute Nodal Coordinates Formulation (ANCF) in Arbitrary Lagrangian Eulerian (ALE) framework. Additionally, a virtual element is introduced to model the contact segment in the cable-pulley system. A tension decay factor is employed to account for the friction in the contact segment. To validate the proposed method, a semi-analytical model based on D’Alembert’s principle is established. Cross-verification is performed to validate the accuracy of both models. The model is further applied to simulate the rotation of the cable-driven manipulator with different structural parameters and frictional factors. The results from the analyses provide valuable guidance for the design and motion control of the in-space cable-driven manipulator. Finally, a prototype of a single module is manufactured and tested. Ground experiments are carried out to verify the kinematic and dynamic models.

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Publication Details

Journal
Chinese Journal of Aeronautics
Published
2025-03-30
DOI
https://doi.org/10.1016/j.cja.2025.103517
Primary Topic
Space Satellite Systems and Control
Type
article
Field-Weighted Citation Impact
0.00

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article

Dynamic modeling and analysis of an in-space cable-driven manipulator for on-orbit servicing

Minghe Shan, Yu Hao Wang, Bo Zhang
Chinese Journal of Aeronautics
Space Satellite Systems and Control
article

Dynamic modeling and analysis of an in-space cable-driven manipulator for on-orbit servicing

Minghe Shan, Yu Hao Wang, Bo Zhang
article en

Abstract

• Kinematics of a cable-driven manipulator is analyzed and its motion planning scheme is designed. • Two dynamic models of the cable-driven manipulator are established and cross-verified. • Tension decay factor is applied to model the frictional contact in cable-pulley systems. • Simulations are performed to investigate the influences of structural parameters on manipulator dynamics. • Ground experiments are carried out to verify the kinematic and dynamic model. In-space cable-driven manipulators exhibit several advantages, such as a large range of motion, high dexterity, and lightweight structure. However, kinematic and dynamic analysis play an essential role in designing a cable-driven manipulator. In this paper, the kinematic analysis of a type of cable-driven manipulator is performed, and a motion planning scheme is conducted to actuate this manipulator. Moreover, a flexible multi-body dynamic model of a cable-driven manipulator considering the frictional contact between the cables and pulleys is established. To describe properties such as flexibility, vibration, and variable length of the cable, this paper utilizes reduced-order beam elements of the Absolute Nodal Coordinates Formulation (ANCF) in Arbitrary Lagrangian Eulerian (ALE) framework. Additionally, a virtual element is introduced to model the contact segment in the cable-pulley system. A tension decay factor is employed to account for the friction in the contact segment. To validate the proposed method, a semi-analytical model based on D’Alembert’s principle is established. Cross-verification is performed to validate the accuracy of both models. The model is further applied to simulate the rotation of the cable-driven manipulator with different structural parameters and frictional factors. The results from the analyses provide valuable guidance for the design and motion control of the in-space cable-driven manipulator. Finally, a prototype of a single module is manufactured and tested. Ground experiments are carried out to verify the kinematic and dynamic models.

Chinese Journal of AeronauticsVol. 39(2)
Beijing Institute of Technology (CN), Zhuhai Institute of Advanced Technology (CN)
National Natural Science Foundation of China, Harbin Institute of Technology, State Key Laboratory of Robotics and System
Decent work and economic growth
Openalex Percentile: Top 92%
Space Satellite Systems and Control
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