An Approach to Spacecraft Returning Reentry Guidance
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    Abstract:

    In this paper,an approach to spacecraft returning reentry guidance is described. The composite shutdown guidance scheme is put forward in the paper,which is applied to decrease reentry state parameters error caused by retro-error in returning phase. And then,reentry guidance law is studied. Finally,it's correctness is proved by simulation.

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History
  • Received:March 14,1997
  • Revised:
  • Adopted:
  • Online: May 28,2014
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