Inverse Kinematics of China Space Station Experimental Module Manipulator

SSRMS refers to a Space Station Remote Manipulator System. The robotic arm of the Wentian module can complete tasks such as supporting astronauts’ extravehicular activities, installing and maintaining payloads, and inspecting the space station. The seven-joint SSRMS manipulator is critical for space missions. This study aims to build its kinematic model via screw theory. It simplifies SSRMS to right-angle rods, defines joint screw axes, twist coordinates, and initial pose matrix. Using the PoE (Product of Exponentials) formula, the 7-DOF forward kinematics equation is derived. In addition, it derives fixed joint angle for inverse kinematics, including analytical solutions and numerical solutions. It elaborates analytical solutions for fixing joints 1/7 and 2/6 and numerical solutions for fixing joints 3/4/5, solves all joint angles via kinematic decoupling, and addresses special cases. Experiments with China’s space station small arm parameters show the probability of meeting the accuracy threshold 10−4 is 99.79%, verifying model effectiveness, while noting singularity-related weak solving areas. This provides a reliable basis for subsequent inverse kinematics optimization.

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Publication Details

Journal
Machines
Published
2026-03-03
DOI
https://doi.org/10.3390/machines14030284
Primary Topic
Space Satellite Systems and Control
Type
article
Field-Weighted Citation Impact
0.00

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article

Inverse Kinematics of China Space Station Experimental Module Manipulator

Yi Yang, Hui Gao, Yuteng Xie, Yonglong Zhang et al.
Machines
Space Satellite Systems and Control
article

Inverse Kinematics of China Space Station Experimental Module Manipulator

Yi Yang, Hui Gao, Yuteng Xie, Yonglong Zhang, Zhiduo Jiang, Zongwu Xie, Mengfei Li, Shuo Zhang, Yuxiang Zhao, Yang Liu
article en

Abstract

SSRMS refers to a Space Station Remote Manipulator System. The robotic arm of the Wentian module can complete tasks such as supporting astronauts’ extravehicular activities, installing and maintaining payloads, and inspecting the space station. The seven-joint SSRMS manipulator is critical for space missions. This study aims to build its kinematic model via screw theory. It simplifies SSRMS to right-angle rods, defines joint screw axes, twist coordinates, and initial pose matrix. Using the PoE (Product of Exponentials) formula, the 7-DOF forward kinematics equation is derived. In addition, it derives fixed joint angle for inverse kinematics, including analytical solutions and numerical solutions. It elaborates analytical solutions for fixing joints 1/7 and 2/6 and numerical solutions for fixing joints 3/4/5, solves all joint angles via kinematic decoupling, and addresses special cases. Experiments with China’s space station small arm parameters show the probability of meeting the accuracy threshold 10−4 is 99.79%, verifying model effectiveness, while noting singularity-related weak solving areas. This provides a reliable basis for subsequent inverse kinematics optimization.

MachinesVol. 14(3)
The University of Sydney (AU), Harbin Institute of Technology (CN)
Natural Science Foundation of Heilongjiang Province
Openalex Percentile: Top 37%
Space Satellite Systems and Control
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Inverse Kinematics of China Space Station Experimental Module Manipulator — Yi Yang, Hui Gao, et al. · Machines (2026) | TGRS Research Map | TGRS