This work was partially supported by the National Natural Science Foundation of China(No.11972182);sponsored by the Qing Lan Project,funded by the Science and Technology on Space Intelligent Control Laboratory(No.KGJZDSYS-2018-11);Postgraduate Research&Practice Innovation Program of Jiangsu Province(No.KYCX200220);Funding for Outstanding Doctoral Dissertation in NUAA(No.BCXJ19-12).The authors fully appreciate their financial supports.
From March 20,2019 to April 30,2019,the 10th China Trajectory Optimization Competition(CTOC10)was jointly held by the Chinese Society of Theoretical and Applied Mechanics and Nanjing University of Aeronautics and Astr...