SHEN Hong-Xin SHEN Hong-Xin

ID:9000263062040

College of Aerospace Science and Engineering, National University of Defense Technology (2013年 CiNii収録論文より)

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  • Hybrid Optimization of Powered Descent Trajectory for Manned Lunar Mission

    PENG Qi-Bo , LI Hai-Yang , SHEN Hong-Xin , TANG Guo-Jin

    The lunar landing stage can be divided into three phases: de-orbit, powered descent and terminal approach. Most fuel is consumed during the powered descent phase. Therefore, the optimization problem o …

    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 56(3), 113-120, 2013-05-04

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