王嘉彬,龙建飞,徐禄祥,吴铭钐,郭 宁,杨 威.闭环控制下单丝扭摆微牛级推力测量系统[J].电子测量与仪器学报,2023,37(9):93-101
闭环控制下单丝扭摆微牛级推力测量系统
Single wire torsion pendulum micro-newton thrust measurement system in closed loop control
  
DOI:
中文关键词:  微牛  电磁力标定  系统参数标定  仿真模拟  微推力测量
英文关键词:micro-Newton  electromagnetic force calibration  system parameter calibration  simulation  micro-thrust measurement
基金项目:国家重点研发计划(2021YFC2202700)、国科大杭州高等研究院自主项目( 2022ZZ01009)、重庆市教委科学技术研项目(KJZDK202101506)、湖南省自然科学基金(2021JJ30564)项目资助
作者单位
王嘉彬 1. 国科大杭州高等研究院基础物理与数学科学学院,2. 中国科学院国家空间科学中心,3. 中国科学院大学,4. 国科大杭州高等研究院引力波太极实验室(杭州),5. 国科大杭州高等研究院浙江省引力波精密测量重点实验室 
龙建飞 1. 国科大杭州高等研究院基础物理与数学科学学院,2. 中国科学院国家空间科学中心,3. 中国科学院大学,4. 国科大杭州高等研究院引力波太极实验室(杭州),5. 国科大杭州高等研究院浙江省引力波精密测量重点实验室 
徐禄祥 1. 国科大杭州高等研究院基础物理与数学科学学院,2. 中国科学院国家空间科学中心,3. 中国科学院大学,4. 国科大杭州高等研究院引力波太极实验室(杭州),5. 国科大杭州高等研究院浙江省引力波精密测量重点实验室 
吴铭钐 1. 国科大杭州高等研究院基础物理与数学科学学院,2. 中国科学院国家空间科学中心,3. 中国科学院大学,4. 国科大杭州高等研究院引力波太极实验室(杭州),5. 国科大杭州高等研究院浙江省引力波精密测量重点实验室 
郭 宁 1. 国科大杭州高等研究院基础物理与数学科学学院 
杨 威 6. 重庆科技学院电气工程学院 
AuthorInstitution
Wang Jiabin 1. School of Fundamental Physics and Mathematical Sciences, Hangzhou Institute for Advanced Study, UCAS,2. National Space Science Centre, Chinese Academy of Sciences,3. University of Chinese Academy of Sciences,Beijing 100049, China; 4. Gravitational Wave Universe Taiji Laboratory,Hangzhou Institute for Advanced Study, UCAS, 5. Key Laboratory of Gravitational Wave Precision Measurement of Zhejiang Province, UCAS 
Long Jianfei 1. School of Fundamental Physics and Mathematical Sciences, Hangzhou Institute for Advanced Study, UCAS,2. National Space Science Centre, Chinese Academy of Sciences,3. University of Chinese Academy of Sciences,Beijing 100049, China; 4. Gravitational Wave Universe Taiji Laboratory,Hangzhou Institute for Advanced Study, UCAS, 5. Key Laboratory of Gravitational Wave Precision Measurement of Zhejiang Province, UCAS 
Xu Luxiang 1. School of Fundamental Physics and Mathematical Sciences, Hangzhou Institute for Advanced Study, UCAS,2. National Space Science Centre, Chinese Academy of Sciences,3. University of Chinese Academy of Sciences,Beijing 100049, China; 4. Gravitational Wave Universe Taiji Laboratory,Hangzhou Institute for Advanced Study, UCAS, 5. Key Laboratory of Gravitational Wave Precision Measurement of Zhejiang Province, UCAS 
Wu Mingshan 1. School of Fundamental Physics and Mathematical Sciences, Hangzhou Institute for Advanced Study, UCAS,2. National Space Science Centre, Chinese Academy of Sciences,3. University of Chinese Academy of Sciences,Beijing 100049, China; 4. Gravitational Wave Universe Taiji Laboratory,Hangzhou Institute for Advanced Study, UCAS, 5. Key Laboratory of Gravitational Wave Precision Measurement of Zhejiang Province, UCAS 
Guo Ning 1. School of Fundamental Physics and Mathematical Sciences, Hangzhou Institute for Advanced Study, UCAS, 
Yang Wei 6. School of Electrical Engineering,Chongqing University of Science and Technology 
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中文摘要:
      针对空间引力波探测任务对微推力测量需求,开发出一套基于闭环控制的单丝扭摆微牛级推力测量系统。 基于扭摆式 微推力测量原理,给出了微推力测量装置详细设计方案,重点分析了扭丝结构、角位移测量、电磁标定力以及闭环控制系统,通 过实验测量对该微推力测量装置进行标定,最后开展误差分析。 测试结果表明,开环状态下扭丝刚度约为 0. 003 25 N·m/ rad, 与理论值误差约 4. 0%;闭环状态下推力测量范围 0. 1~ 246. 0 μN,最小分辨率优于 0. 1 μN,相对不确定误差为 1. 174%,满足对 微推力器推力测量范围、分辨率和精度的测量要求。
英文摘要:
      In response to the micro-newton thrust measurement requirements for space gravitational wave detection missions, a singlewire torsion micro-newton thrust measurement system based on closed-loop control has been developed. Based on the principle of torsional pendulum micro-newton thrust measurement, the detailed design scheme of the micro-newton thrust measurement device is given, and the twisted wire structure, angular displacement measurement, electromagnetic calibration force, and closed-loop control system are mainly analyzed. The micro-newton thrust measuring device is calibrated through experimental measurement, and finally the error analysis is carried out. The test results show that the torsion wire stiffness is about 0. 003 25 N·m/ rad in the open-loop state, and the error with the theoretical value is about 4. 0%; the thrust measurement range in the closed-loop state is 0. 1 ~ 246. 0 μN, and the minimum resolution is better than 0. 1 μN, which is relatively uncertainty error is 1. 174%, which meets the measurement requirements for the thrust measurement range, resolution and accuracy of micro thrusters.
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