Volume 35 Issue 5
Sep.  2015
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LIU Hailong, HAN Xu, SHI Xiaoping. Attitude And Translation Control For Spacecraft To Approach To A Tumbling Non-Cooperative Object During The Final Phase[J]. Chinese Journal of Space Science, 2015, 35(5): 603-610. doi: 10.11728/cjss2015.05.603
Citation: LIU Hailong, HAN Xu, SHI Xiaoping. Attitude And Translation Control For Spacecraft To Approach To A Tumbling Non-Cooperative Object During The Final Phase[J]. Chinese Journal of Space Science, 2015, 35(5): 603-610. doi: 10.11728/cjss2015.05.603

Attitude And Translation Control For Spacecraft To Approach To A Tumbling Non-Cooperative Object During The Final Phase

doi: 10.11728/cjss2015.05.603
  • Received Date: 2014-07-26
  • Rev Recd Date: 2015-03-02
  • Publish Date: 2015-09-15
  • This paper considers the process of motion synchronization of chaser satellite and target satellite in space. The problem of final approach to a non-cooperative tumbling target is studied in this paper. The accurate orbit and attitude dynamics model of two relative motion spacecrafts with arbitrary eccentrics is established. In order to insure the safety of final approach, the traditional linear synchronization rotating approach strategy is improved by designing an exponential decay reference trajectory to decay relative velocity with decreasing relative distance and reach zero when the chaser is hovering. The proportional-derivative-decouple relative attitude controller and relative orbit controller is proposed. The simulation shows the process of the relative velocity of the chaser decay to zero. The stability of the control law is demonstrated through Lyapunov analysis and effectiveness of controller is verified by the numerical simulation.

     

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