Technical Papers
Jan 31, 2024

Development of a High-Accuracy Inertia Simulation System for Drive Joints of Space Station Transfer Arm

Publication: Journal of Aerospace Engineering
Volume 37, Issue 3

Abstract

With a focus on crewed spaceflight and space station construction, this research developed a high-accuracy inertia simulation system for the drive joints of the space station transfer arm. To achieve this objective, both mechanical inertia and electric inertia simulation methods were utilized. To enhance the dynamic characteristics of the electric inertia simulation system, a rigorous electric inertia simulation model was developed, and a comprehensive controller, along with a feedforward controller based on the structure invariance principle, was designed. The simulation results demonstrated that the controller significantly enhances the control performance of the system, with extraneous torque being suppressed by more than 95%. The mechanical inertia simulation method accurately models the invariant inertia, whereas the electric inertia simulation method can precisely simulate the time-varying inertia. To validate the effectiveness of the simulation system, experiments were conducted. The results confirm that the electric inertia simulation method is comparable to the mechanical inertia simulation method in aerospace engineering applications. The simulation performance of the electric inertia simulation system for both constant and time-varying inertia is excellent.

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Data Availability Statement

Some or all data, models, or codes that support the findings of this study are available from the corresponding author upon reasonable request.

Acknowledgments

This research work is supported by the National Natural Science Foundation of China (No. 51105094).

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Journal of Aerospace Engineering
Volume 37Issue 3May 2024

History

Received: Aug 1, 2023
Accepted: Oct 27, 2023
Published online: Jan 31, 2024
Published in print: May 1, 2024
Discussion open until: Jun 30, 2024

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Doctoral Student, School of Mechatronics Engineering, Harbin Institute of Technology, Harbin 150001, China. Email: [email protected]
Qitao Huang [email protected]
Professor, School of Mechatronics Engineering, Harbin Institute of Technology, Harbin 150001, China (corresponding author). Email: [email protected]
Tianfang Xu [email protected]
Researcher, Shanghai Electro-Mechanical Engineering Institute, China Aerospace Science and Technology Corporation (CASC), Shanghai 201109, China. Email: [email protected]
Researcher, Shanghai Institute of Aerospace System Engineering, China Aerospace Science and Technology Corporation (CASC), Shanghai 201109, China. Email: [email protected]
Hongguang Xu [email protected]
Professor, School of Mechatronics Engineering, Harbin Institute of Technology, Harbin 150001, China. Email: [email protected]

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