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Research Progress of the Structure Vibration-Attitude Coordinated Control of Spacecraft

  • Yang, Jingyu (Laboratory of Space Solar Power Station Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • Qu, Shiying (Laboratory of Space Solar Power Station Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • Lin, Jiahui (Laboratory of Space Solar Power Station Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • Liu, Zhiqi (Laboratory of Space Solar Power Station Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • Cui, Xuanming (Laboratory of Space Solar Power Station Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • Wang, Chu (Laboratory of Space Solar Power Station Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • Zhang, Dujiang (Laboratory of Space Solar Power Station Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • gu, Mingcheng (Laboratory of Space Solar Power Station Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • Sun, Zhongrui (Laboratory of Space Solar Power Station Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • Yang, Kang (Laboratory of Space Solar Power Station Dynamics and Control, Faculty of Aerospace Engineering, Shenyang Aerospace University) ;
  • Zhou, Lanwei (The State Key Laboratory of Mechanics and Control for Mechanical Structures, Nanjing University of Aeronautics and Astronautics) ;
  • Chen, Guoping (The State Key Laboratory of Mechanics and Control for Mechanical Structures, Nanjing University of Aeronautics and Astronautics)
  • Received : 2015.05.27
  • Accepted : 2015.12.15
  • Published : 2015.12.30

Abstract

This paper gives an overview of research on the field of structure vibration-attitude coordinated control of spacecraft. First of all, the importance of the technology has been given an introduction, and then later the research progress of space structure dynamics modeling, research progress of structure vibration-attitude coordinated control of flexible spacecraft have been discussed respectively. Finally, future research on application of structure vibration-attitude coordinated control of spacecraft has been recommended.

Keywords

spacecraft;vibration-attitude coordinated control;overview

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