Volume 38 Issue 6
Nov.  2018
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Article Navigation >  Chinese Journal of Space Science  > 2018  >  38(6): 925-933
WANG Youliang, ZHENG Jianhua, LI Mingtao. Analytical Formation Keeping Control Strategy for Micro-satellites[J]. Chinese Journal of Space Science, 2018, 38(6): 925-933. doi: 10.11728/cjss2018.06.925
Citation: WANG Youliang, ZHENG Jianhua, LI Mingtao. Analytical Formation Keeping Control Strategy for Micro-satellites[J]. Chinese Journal of Space Science, 2018, 38(6): 925-933. doi: 10.11728/cjss2018.06.925
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Analytical Formation Keeping Control Strategy for Micro-satellites

doi: 10.11728/cjss2018.06.925

  • National Space Science Center, Chinese Academy of Sciences, Beijing 100190;Key Laboratory of Electronics and Information Technology for Space Systems, Chinese Academy of Sciences, Beijing 100190;University of Chinese Academy of Sciences, Beijing 100049

  • Received Date: 2017-09-15
  • Rev Recd Date: 2018-04-23
  • Publish Date: 2018-11-15
    Abstract
  • Formation keeping is the foundation of satellite formation flying. J2 term and atmospheric drag are the main perturbations for the low Earth orbit satellites, which can cause the long-term change of relative velocity and formation drift. Firstly, the mean relative velocity is used to denote the drift rate of satellite formation, and the analytical representation between the mean relative velocity and impulse maneuver is derived. Then the mean relative acceleration is developed, and the relative motion under the main perturbations is equivalent to a uniformly accelerated motion. Finally, it is combined with the single side limit cycle control method, and an analytical formation keeping control strategy based on the inter-satellite ranging information is designed. The numerical simulation results indicate that the strategy is simple and effective, which is easy to implement in engineering and suitable to the autonomous control for micro-satellites especially.

     

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