高级搜索

留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

航天器相对运动地面动力学实验研究

齐彧,  孙俊,  师鹏,  赵育善

downloadPDF
文章导航 > 北京航空航天大学学报  > 2016 >  42(10): 2118-2129.
齐彧, 孙俊, 师鹏, 等 . 航天器相对运动地面动力学实验研究[J]. 北京航空航天大学学报, 2016, 42(10): 2118-2129. doi: 10.13700/j.bh.1001-5965.2015.0637
引用本文: 齐彧, 孙俊, 师鹏, 等 . 航天器相对运动地面动力学实验研究[J]. 北京航空航天大学学报, 2016, 42(10): 2118-2129. doi: 10.13700/j.bh.1001-5965.2015.0637
shu
QI Yu, SUN Jun, SHI Peng, et al. Research for ground-based astrodynamical experiment for spacecraft relative motion[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(10): 2118-2129. doi: 10.13700/j.bh.1001-5965.2015.0637(in Chinese)
Citation: QI Yu, SUN Jun, SHI Peng, et al. Research for ground-based astrodynamical experiment for spacecraft relative motion[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(10): 2118-2129. doi: 10.13700/j.bh.1001-5965.2015.0637(in Chinese)
shu

航天器相对运动地面动力学实验研究

doi: 10.13700/j.bh.1001-5965.2015.0637
  • 1.

    北京航空航天大学 宇航学院, 北京 100083

  • 2. 上海航天控制技术研究所, 上海 20023

  • 3. 上海市空间智能控制技术实验室, 上海 200233

基金项目: 国家自然科学基金（11572019）；上海航天创新基金（SAST2015078）
详细信息
    作者简介:

    齐彧,男,博士研究生。主要研究方向:航天器地面实验、航天器姿轨控制。Tel.:010-82339286,E-mail:15811425613@163.com;赵育善,男,博士,教授,博士生导师。主要研究方向:航天器轨道动力学。Tel.:010-82317339,E-mail:yszhao@buaa.edu.cn

    通讯作者:

    赵育善,Tel.:010-82317339,E-mail:yszhao@buaa.edu.cn

  • 中图分类号: V416.2

Research for ground-based astrodynamical experiment for spacecraft relative motion

  • 1.

    School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • 2. Shanghai Aerospace Control Technology Institute, Shanghai 20023

  • 3. Shanghai Key Laboratory of Aerospace Intelligent Control Technology, Shanghai 200233, China

Funds: National Natural Science Foundation of China (11572019); Spacecraft Innovation Foundation of Shanghai (SAST2015078)

    摘要
  • 摘要: 研究了航天器相对运动地面动力学实验的构建问题及实验结果的可信性问题。首先利用相似性理论给出了航天器相对运动地面动力学实验的建立方法，而后针对地面实验环境与空间真实环境之间的力学环境差异提出补偿办法，之后针对航天器相对运动地面动力学实验中的干扰因素进行分析并给出相应的补偿策略，然后利用动力学等效性建立航天器相对运动地面动力学实验控制策略，该控制策略中包括力学差异补偿以及实验环境干扰补偿，数值仿真结果与地面实验结果均证明该控制策略能够满足地面实验要求，最后以相似性理论为依托建立相似性度量函数，并利用这一函数证明了航天器相对运动地面实验结果的可信性。仿真结果表明，给出的航天器相对运动地面动力学实验方案可行，其实验结果可信，对地面实验的开展具有重要的参考价值。

     

    Abstract: This paper proposes a method to build the spacecraft relative motion's ground-based astrodynamical experiment and figures out an approach to prove the reliability of ground-based experimental results. First, the spacecraft relative motion's ground-based astrodynamical experiment is carried out with the help of similarity theory, then the compensation method for making up the dynamical difference between space environment and experimental environment, after that the dynamical model of experimental disturbances is given for further counteract. Second, an experimental control method similar to space control system is designed for controlling the relative motion and compensating the inertia forces, and both the numerical simulation and experimental results show the effectiveness of control system. Finally, a similarity function used for measuring the similarity degree of experimental result will be helpful in proving the reliability of spacecraft relative motion's ground-based astrodynamical experiment. According to the results of simulation, the experimental scheme is available and reliable. This method is helpful for the development of ground-based astrodynamical experiment.

     

    • HTML全文
    • 参考文献(19)
  • [1] REZAEEPAZH J,YAZDI A.Similitude requirements and scaling laws for flutter prediction of angle-ply composite plates[J].Composites:Part B,2010,42(1):51-56.
    [2] TORKAMANI S,NAVAZI H M,JAFARI A A.Structural similitude in free vibration of orthogonally stiffened cylindrical shells[J].Thin-Walled Structure,2009,47(11):1316-1330.
    [3] AKIN D L,HOWARD R D.Telerobotic operations testing in neutral buoyancy simulation[C]//Proceedings 4th Annual Conference on Intelligent Robotic Systems for Space Exploration.Piscataway,NJ:IEEE Press,1992:42-49.
    [4] SINGER S M,AKIN D L.Scheduling robot task performance for a cooperative human and robotic team[J].Acta Astronautica,2010,66(1-2):102-116.
    [5] 崔俊峰,冯咬齐,于丹,等.航天器动力学环境试验综合测试系统的设计[J].计算机测量与控制,2006,20(3):363-364.CUI J F,FENG Y Q,YU D,et al.The design of intergrated measurement system for spacecraft dynamic environment testing[J].Computer Measurement and Control,2006,20(3):363-364(in Chinese).
    [6] 李大琪,沈均毅,陈宏敏.航天员呼吸强度的时序模式相似性比较研究[J].宇航学报,2008,29(3):971-976.LI D Q,SHEN J Y,CHEN H M.Study on similarity comparison of sequential pattern of astronaut's respiratory intensity[J].Journal of Astronautics,2008,29(3):971-976(in Chinese).
    [7] WAKI H,SHIMIZU T,KATAHIRA K,et al.Effects of microgravity elicited by parabolic flight on abdominal aortic pressure and heart rate in rats[J].Journal of Applied Physiology,2002,93(6):1893-1899.
    [8] 何兆伟,师鹏,葛冰,等.航天器地面实验的相似性分析方法[J].北京航空航天大学学报,2012,38(4):502-508.HE Z W,SHI P,GE B,et al.Similitude investigation for ground experiment of spacecraft[J].Journal of Beijing University of Aeronautics and Astronautics,2012,38(4):502-508(in Chinese).
    [9] 周美立.相似性科学[M].北京:科学出版社,2004:81-154.ZHOU M L.Similarity science[M].Beijing:Science Press,2004:81-154(in Chinese).
    [10] BARNETT R,CHRISTOPHER T.Similarity[M].New York:McGraw-Hill Professional,2013:35-73.
    [11] JANA L S,MASON A P,CHRISTOPHER D H.Historical review of air-bearing spacecraft simulators[J].Journal of Guidance,Control,and Dynamics,2003,26(4):513-522.
    [12] GINN J S.Spacecraft formation flight:Analysis of the perturbed J2-modified Hill-Clohessy-Wiltshire equations[J].Aerospace Engineering,2007,3(3):193-198.
    [13] 赵育善,师鹏.航天器飞行动力学建模理论与方法[M].北京:北京航空航天大学出版社,2004:181-189.ZHAO Y S,SHI P.Theory and method for spacecraft flight dynamics modeling[M].Beijing:Beihang University Press,2004:181-189(in Chinese).
    [14] WIGBERT F.Automated rendezvous and docking of spacecraft[M].Cambridge:Cambridge University Press,2003:342-381.
    [15] 许剑,任迪,杨庆俊,等.五自由度气浮仿真试验台的动力学建模[J].宇航学报,2010,31(1):60-64.XU J,REN D,YANG Q J,et al.Dynamic modeling for the 5-DoF air bearing spacecraft simulator[J].Journal of Astronautics,2010,31(1):60-64(in Chinese).
    [16] 姜静,孟利东.线性二次型最优控制器的设计[J].软件工程与应用,2014,3(13):97-103.JIANG J,MENG L D.The design of linear quadratic optimal controller[J].Software Engineering and Applications,2014,3(13):97-103(in Chinese).
    [17] HERNANDEZ O,ORTIZ P,HERRERA J.Fractional PID controller with LQR proportional action applied to fractional model of cement rotary kiln[J].Latin America Transactions IEEE,2015,13(1):37-42.
    [18] LOVELL T A,SPENCER D A.Relative orbital elements formulation based upon the Clohessy-Wiltshire equations[J].Journal of the Astronautical Sciences,2015,17(1):270-278.
    [19] 李保军,师鹏,张皓,等.卫星编队的多脉冲队形重构方法[J].北京航空航天大学学报,2009,35(8):950-952.LI B J,SHI P,ZHANG H,et al.Satellites formation reconfiguration with multiple impulses[J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(8):950-952(in Chinese).
    • 相关文章
    • 施引文献
  • 资源附件(0)
  • 加载中
WeChat 点击查看大图
计量
  • 文章访问数:  817
  • HTML全文浏览量:  22
  • PDF下载量:  821
  • 被引次数: 0
出版历程
  • 收稿日期:  2015-09-26
  • 网络出版日期:  2016-10-20

目录

    /

    返回文章
    返回
    常见问答

    版权所有 © 《北京航空航天大学学报》编辑部

    通讯地址：北京市海淀区学院路37号 《北京航空航天大学学报》编辑部　 邮编：100191 邮箱：jbuaa@buaa.edu.cn

    本系统由 北京仁和汇智信息技术有限公司 开发    百度统计