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Control validation of a five-degree-of-freedom motion platform

  • Beijing Institute of Technology
  • CAS - Institute of Mechanics
  • Northeastern University China

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

To meet the in-orbit testing requirements for spacecraft hardware and software while enhancing the reliability of ground-based five-degree-of-freedom motion platform, a novel ground-based five-degree-of-freedom motion platform was developed for testing various spacecraft subsystems. Based on the platform's dynamic characteristics, a PID controller designed to prevent differential kick was developed. This controller effectively mitigates the effects of differential kick on the system during the initial operation phase. Experiments conducted on the five-degree-of-freedom motion platform validated the platform's position and attitude degrees of freedom functionality. Results demonstrate that the system accurately achieves tracking capabilities, with controller outputs free of differential chatter. This ensures system stability, providing a reliable platform and control solution for spacecraft ground simulation.

源语言英语
主期刊名Fifth International Conference on Computer Technology, Information Engineering, and Electron Materials, CTIEEM 2025
编辑Ming Diao, Mas Rina Mustaffa
出版商SPIE
ISBN(电子版)9798902322405
DOI
出版状态已出版 - 8 4月 2026
已对外发布
活动5th International Conference on Computer Technology, Information Engineering, and Electron Materials, CTIEEM 2025 - Harbin, 中国
期限: 12 12月 202514 12月 2025

出版系列

姓名Proceedings of SPIE - The International Society for Optical Engineering
14139
ISSN(印刷版)0277-786X
ISSN(电子版)1996-756X

会议

会议5th International Conference on Computer Technology, Information Engineering, and Electron Materials, CTIEEM 2025
国家/地区中国
Harbin
时期12/12/2514/12/25

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