Generalized multiple-revolution Lambert algorithm for solving multiple-impulse rendezvous problem

[1] Battin R H. An introduction to the mathematics and methods of astrodynamics[M].New York: AIAA, 1987:237-342 [2] 韩潮,谢华伟. 空间交会中多圈Lambert变轨算法研究[J]. 中国空间科学技术, 2004, 24(5): 9-14 Han Chao, Xie Huawei. Research on algorithm of loopy Lambert transfer in space rendezvous[J].Chinese Space Science and Technology, 2004, 24(5): 9-14 (in Chinese) [3] 卢山,陈统,徐世杰. 基于自适应模拟退火遗传算法的最优Lambert转移[J].北京航空航天大学学报, 2007, 33(10): 1191-1195 Lu Shan, Chen Tong, Xu Shijie. Optimal Lambert transfer based on adaptive simulated annealing genetic algorithm[J].Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(10):1191-1195(in Chinese) [4] Loechler L A. An elegant Lambert algorithm for multiple revolution orbits .Massachusetts: Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, 1988 [5] Shen H J, Tsiotras P. Optimal two-impulse rendezvous using multiple-revolution Lambert solutions[J].Journal of Guidance, Control, and Dynamics, 2003, 26(1):50-61 [6] Prussing J E. A class of optimal two-impulse rendezvous using multiple-revolution Lambert solutions[J].The Journal of the Astronautical Sciences, 2000, 48(2):131-148 [7] Shen H J. Optimal scheduling for satellite refuelling in circular orbits .Georgia: School of Aerospace Engineering, Georgia Institute of Technology, 2003 [8] Hughes S P, Mailhe L M, Guzman J J. A comparison of trajectory optimization methods for the impulsive minimum fuel rendezvous problem[J].Advances in the Astronautical Sciences, 2003, 113:85-104 [9] Luo Yazhong, Tang Guojing, Lei Yongjun, et al. Optimization of multiple-impulse multiple-revolution rendezvous phasing maneuvers[J].Journal of Guidance, Control, and Dynamics, 2007, 30(4):946-952 [10] Xie Xiaofeng, Zhang Wenjun. Solving engineering design problems by social cognitive optimization Kalyanmov D, Riccardo P.Genetic and Evolutionary Computation Conference. Berlin:Springer, 2004:261-262 [11] 童科伟,周建平,何麟书.近地卫星简化轨道预报方法研究[J].宇航学报,2009,30(4):1327-1333 Tong Kewei, Zhou Jianping, He Linshu. A reduced orbit propagation model of low-earth orbit satellite[J].Journal of Astronautics, 2009, 30(4):1327-1333(in Chinese)