• CN:11-2187/TH
  • ISSN:0577-6686

机械工程学报 ›› 2021, Vol. 57 ›› Issue (3): 11-25.doi: 10.3901/JME.2021.03.011

• 机器人及机构学 • 上一篇    下一篇

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空间可展开天线微重力环境模拟研究现状与展望

田大可1, 范小东1, 郑夕健1, 刘荣强2, 郭宏伟2, 邓宗全2   

  1. 1. 沈阳建筑大学机械工程学院 沈阳 110168;
    2. 哈尔滨工业大学机电工程学院 哈尔滨 150001
  • 收稿日期:2020-02-18 修回日期:2020-07-22 出版日期:2021-02-05 发布日期:2021-03-16
  • 通讯作者: 郑夕健(通信作者),男,1963年出生,博士,教授,硕士研究生导师。主要研究方向为宇航空间机构及控制、建筑机械设计与产品开发等。E-mail:xijianzheng@sina.com
  • 作者简介:田大可,男,1981年出生,博士,副教授,硕士研究生导师。主要研究方向为空间可展开机构创新设计理论与方法、航空发动机总体结构及先进技术。E-mail:tiandake@sjzu.edu.cn;范小东,男,1995年出生,硕士研究生。主要研究方向为机构学及宇航空间可展开机构。E-mail:fanxiaodong@stu.sjzu.edu.cn
  • 基金资助:
    国家自然科学基金重点(51835002)、中国博士后科学基金面上(2019M661126)和辽宁省自然基金指导计划(2019-ZD-0655)资助项目。

Research Status and Prospect of Micro-gravity Environment Simulation for Space Deployable Antenna

TIAN Dake1, FAN Xiaodong1, ZHENG Xijian1, LIU Rongqiang2, GUO Hongwei2, DENG Zongquan2   

  1. 1. School of Mechanical Engineering, Shenyang Jianzhu University, Shenyang 110168;
    2. School of Mechanical and Electrical Engineering, Harbin Institute of Technology, Harbin 150001
  • Received:2020-02-18 Revised:2020-07-22 Online:2021-02-05 Published:2021-03-16

摘要: 为满足我国深空探测、空间站建设、探月工程等重大航天工程对空间大型可展开天线等新型卫星有效载荷平台快速发展的要求,对国内外空间可展开天线微重力环境模拟方法进行了综述。分别对落塔法、抛物线飞行法、水浮法、气浮法和悬吊法等典型重力补偿方法的工作原理及优缺点进行了分析,综述了国内外在此领域的应用及技术发展情况,综合分析并比较了5种微重力模拟方法的技术特点及适用范围,结合我国航天科技中长期发展规划的需求,从大型化、高精度化、多样化、通用化、高保真化等方面,提出了未来可展开天线微重力模拟的发展趋势及方向,旨在为我国大型可展开天线及其微重力环境模拟方法的基础理论研究及工程应用提供借鉴与参考。

关键词: 空间可展开天线, 微重力环境模拟, 卸载方法, 微重力水平, 试验系统

Abstract: In order to meet the requirements of China's deep space exploration, space station construction, lunar exploration and other major aerospace projects for the rapid development of large space deployable antennas and other new satellite payload platforms, the micro-gravity environment simulation methods of space deployable antenna at home and abroad are reviewed. The working principle, advantages and disadvantages of typical gravity compensation methods, such as drop tower method, parabolic flight method, neutral buoyancy method, air floating method and suspension method, are analyzed respectively. The application and technical development in this field at home and abroad are reviewed. The technical characteristics and application scope of five micro-gravity simulation methods are analyzed and compared. Considering the needs of Chinese medium and long-term development plan for space science and technology, and from the aspects of large scale, high precision, diversification, generalization and high fidelity, the development trend and direction of micro-gravity environment simulation for space deployable antenna are proposed. The review provides a reference for the basic theoretical research and engineering application of large deployable antenna and micro-gravity environment simulation methods in China.

Key words: deployable antenna, micro-gravity environment simulation, unloading method, micro-gravity level, experimental system

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