从哈勃太空望远镜剖析微振动对高性能航天器指向测量与控制系统的影响

李林; 袁利; 王立; 郑然; 王晓燕; 武延鹏

doi:10.37188/OPE.20202811.2478

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从哈勃太空望远镜剖析微振动对高性能航天器指向测量与控制系统的影响

微纳技术与精密机械 | 更新时间：2020-12-09

- 从哈勃太空望远镜剖析微振动对高性能航天器指向测量与控制系统的影响
- Influence of micro vibration on measurement and pointing control system of high-performance spacecraft from Hubble Space Telescope
- 光学精密工程 2020年28卷第11期页码：2478-2487
- 作者机构：
  
  1.北京控制工程研究所空间光电测量与感知实验室, 北京 100190
  2.空间智能控制技术重点实验室, 北京 100094
  3.中国空间技术研究院, 北京 100190
- 作者简介：
  
  [ "李林(1990-), 男, 湖北郧阳人, 博士, 助理研究员, 2018年于中国科学院大学获得博士学位, 主要从事空间态势感知、极高精度指向测量技术以及航天器微振动技术等方面的研究。E-mail:cast_lilin@163.com" ]
  [ "袁利(1974-), 男, 博士, 研究员, 北京控制工程研究所所长, 空间智能控制技术重点实验室主任, 中国宇航学会、中国空间科学学会等多个学会理事, 长期从事航天器姿态控制和光学敏感器方面的研究工作" ]
- 基金信息：
  
  国家自然科学基金资助项目(51905034);国家自然科学基金资助项目(11903004);国防重点基础研究项目
- DOI：10.37188/OPE.20202811.2478
  中图分类号： V423.4
- 收稿日期：2020-05-06，
  
  修回日期：2020-07-02，
  
  录用日期：2020-7-2，
  
  纸质出版日期：2020-11-25
- 稿件说明：
移动端阅览
李林, 袁利, 王立, 等. 从哈勃太空望远镜剖析微振动对高性能航天器指向测量与控制系统的影响[J]. 光学精密工程, 2020,28(11):2478-2487.

Lin LI, Li YUAN, Li WANG, et al. Influence of micro vibration on measurement and pointing control system of high-performance spacecraft from Hubble Space Telescope[J]. Optics and precision engineering, 2020, 28(11): 2478-2487.
李林, 袁利, 王立, 等. 从哈勃太空望远镜剖析微振动对高性能航天器指向测量与控制系统的影响[J]. 光学精密工程, 2020,28(11):2478-2487. DOI： 10.37188/OPE.20202811.2478.

Lin LI, Li YUAN, Li WANG, et al. Influence of micro vibration on measurement and pointing control system of high-performance spacecraft from Hubble Space Telescope[J]. Optics and precision engineering, 2020, 28(11): 2478-2487. DOI： 10.37188/OPE.20202811.2478.

摘要

本文综述了极限性能哈勃太空望远镜（Hubble Space Telescope，HST）在轨微振动的研究进展，说明了其指向测量与控制系统组成和特点，同时给出了其关键技术指标，有针对性地剖析了HST在高性能航天器微振动研究及指向控制技术等方面的先进技术和理念。阐述了HST反作用轮组件、太阳电池阵的扰动特点以及微振动引起光学元件抖动的现象，在此基础上，对现代航天器5种先进指向控制技术进行了总结，包括基于降阶模型的控制、基于线性二次高斯的控制、解析和数值推导的

∞控制、协方差控制和双模干扰调节控制。HST微振动相关技术分析方法可为我国高分专项、深空探测、载人航天、引力波探测等涉及到的高性能航天器、毫角秒级敏感器以及空间站光学舱等高精度光学仪器的研制、地面试验和在轨干扰环境量化评估提供有益的借鉴。

Abstract

The micro vibration study of the famous Hubble Space Telescope (HST)

which is known for its superior in-orbit performance

was reviewed

the composition and characteristics of its pointing control system (PCS) were explained

and the key technical indexes were listed. The study analyzed the application of the advanced technology and concept of HST in the research of micro vibrations and high-performance PCS technology. The disturbance characteristics of the HST Reaction wheel assemblies (RWAs)

Solar Array (SA)

and the phenomenon of optical element jitter caused by micro vibrations were expounded

based on which five advanced pointing control technologies of modern spacecrafts were summarized

including Reduced-Order Model-Based Control Design

Linear Quadratic Gaussian-Based Controller Design

Analytically and Numerically Derived

∞ Controller Designs

Covariance Control Design

and Dual-Mode Disturbance-Accommodating Controller Design. The data gathered from this analysis and the experience can provide a valuable experience for high-performance spacecrafts that use RWA

CMG

and other potential disturbance sources. The HST micro vibration technologies and analysis methods can provide effective references for the development of high-precision optical instruments

such as high-performance spacecrafts

millisecond optical sensors

and Guangxuecang of space station

ground test

and in-orbit interference environment quantitative assessment

which are involved in the Gaofeng project

Deep Space Exploration

Manned Spaceflight

and Gravitational Wave Detection in China.

关键词

Keywords

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