首页 | 本学科首页   官方微博 | 高级检索  
     

高精度低连接刚度大惯量扫描镜控制系统设计
引用本文:闵溢龙,王淦泉. 高精度低连接刚度大惯量扫描镜控制系统设计[J]. 宇航学报, 2021, 42(2): 220-229. DOI: 10.3873/j.issn.1000-1328.2021.02.010
作者姓名:闵溢龙  王淦泉
作者单位:1. 中国科学院大学,北京 100049;2. 中国科学院上海技术物理研究所,上海 200083;3.中国科学院红外探测与成像技术重点实验室,上海 200083
基金项目:中国科学院青年创新促进会人才计划(Y201951)
摘    要:针对三轴稳定卫星内低连接刚度条件下的大惯量扫描镜负载在低速摆动时易出现机械谐振的问题,基于电流-速度-位置三闭环控制结构,研究并提出一种有效的易于工程实现的优化控制方法,抑制机械谐振同时提高扫描镜系统的控制性能.首先,根据动力学关系对低刚度连接的电机与扫描镜控制对象建立理论的简化控制模型.然后,分析加速度反馈抑制谐振、...

关 键 词:三轴稳定卫星  大惯量负载  扫描镜  机械谐振  运动控制  控制性能  加速度观测器
收稿时间:2020-02-05

Design of High Accuracy Scanning Mirror Control Systemwith LargeInertia and Low Stiffness Connection
MIN Yi long,WANG Gan quan. Design of High Accuracy Scanning Mirror Control Systemwith LargeInertia and Low Stiffness Connection[J]. Journal of Astronautics, 2021, 42(2): 220-229. DOI: 10.3873/j.issn.1000-1328.2021.02.010
Authors:MIN Yi long  WANG Gan quan
Affiliation:1. University of Chinese Academy of Sciences, Beijing100049, China; 2. Shanghai Institute of Technical Physics of theChinese Academy of Sciences, Shanghai 200083, China; 3. CAS Key Laboratory ofInfrared System Detection and Imaging Technology,Shanghai 200083, China
Abstract:For a three axis stabilized satellite, themechanical resonance caused by high inertia load and low stiffness connectionis easy to occur in its low speed scanning mirror motion control system. Basedon the current speed positioncontrol structure, an optimized control method that is effective and easy to beimplemented in engineering is investigated and proposed. The mechanicalresonance is suppressed and the control performance is improved for thescanning mirror system. Firstly, a theoretical simplified control model isestablished based on the dynamic relationship between the low stiffnesscoupling system of the motor and the large inertia scanning mirror. Then, weanalyze the reason that the acceleration feedback suppresses the resonance andimproves the control ability of the system, use the current and positionfeedback signals to establish an acceleration observer to obtain the motoracceleration and feedback, and analyze the optimization effect of the method bysimulation. Finally, we carry out the experimental verification on an actualsystem and compare the changes of the system control errors. The experimentalresults show that the proposed control method can effectively suppress themechanical resonance, and increase the bandwidth and dynamic accuracy of themotion control system.
Keywords:
本文献已被 CNKI 等数据库收录!
点击此处可从《宇航学报》浏览原始摘要信息
点击此处可从《宇航学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号