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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陈克俊.飞船返回再入制导方法研究[J].国防科技大学学报,1997,19(6):31-35. Chen Kejun. An Approach to Spacecraft Returning Reentry Guidance[J]. Journal of National University of Defense Technology,1997,19(6):31-35.