[1]GOBETZ F W, DOLL J R. A survey of impulsive trajectories [J]. AIAA Journal, 1969, 7(5): 801834.
[2]杨嘉墀. 航天器轨道动力学与控制(下)[M]. 北京:宇航出版社, 2002:61137.
[3]唐国金, 罗亚中, 雍恩米. 航天器轨迹优化理论、方法及应用[M]. 北京:科学出版社, 2012:167195.
[4]PRUSSING J E, CHIU J H. Optimal multipleimpulse timefixed rendezvous between circular orbits [J]. Journal of Guidance Control and Dynamics, 1986, 9(1):1722.
[5]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: 85104.
[6]LUO Y Z, TANG G J, LEI Y J, et al. Optimization of multipleimpulse multiplerevolution rendezvous phasing maneuvers [J]. Journal of Guidance, Control and Dynamics, 2007, 30(4): 946952.
[7]ABDELKHALIK O, MORTARI D. Nimpulse orbit transfer using genetic algorithms [J]. Journal of Spacecraft and Rockets, 2007, 44(2): 456460.
[8]ABDELKHALIK O. Orbit design and estimation for surveillance missions using genetic algorithms [D]. Austin: University of Texas, 2005.
[9]KENNEDY J, EBERHART R. Particle swarm optimization [C]// IEEE International Conference on Neural Networks. New York: IEEE, 1995:19421948.
[10]ZHU K J, JIANG F H, LI J F, et al. Trajectory optimization of multiasteroids exploration with low thrust [J]. Transactions of the Japan Society for Aeronautical and Space Sciences, 2009, 52: 4754.
[11]PONTANI M, GHOSH P, CONWAY B A. Particle swarm optimization of multipleburn rendezvous trajectories [J]. Journal of Guidance, Control, and Dynamics, 2012, 35(4): 11921207.
[12]VALLADO D A. Fundamentals of astrodynamics and applications [M].2nd ed. EI Segundo, California: Microcosm Press, 2001:303395.
[13]BROWN C D. Spacecraft mission design [M]. 2nd ed. Washington D.C.:AIAA, 1998: 3951. |