多脉冲异面交会对接转移轨道的优化
刘源, 叶潇, 郝勇, 李玉玲. 多脉冲异面交会对接转移轨道的优化[J]. 光学 精密工程, 2017, 25(4): 987.
LIU Yuan, YE Xiao, HAO Yong, LI Yu-ling. Optimization of transfer orbit for multiple-pulse noncoplanar rendezvous and docking[J]. Optics and Precision Engineering, 2017, 25(4): 987.
[1] 崔乃刚, 王平, 郭继峰, 等. 空间在轨服务技术发展综述[J]. 宇航学报, 2007,28(4): 805-811.
CUI N G, WANG P, GUO J F, et al.. A review of on-orbit servicing [J]. Journal of Astronautics.2007,28(4): 805-811.(in Chinese)
[2] TAUR D R,COVERSTONE-CARROL V, PRU-SSING J E. Optimal impulsive time-fixed orbital rendezvous and interception with path constraints [J]. Journal of Guidance Control and Dynamics, 1995,18(1): 54-60.
[3] 赵琳,李玉玲,刘源,等. 连续小推力拦截卫星攻击轨道的优化[J].光学 精密工程,2016,24(1): 178-186.
[4] LAWDEN D F. Optimal Trajectories for Space Navigation [M]. London: Butterworths ,1963.
[5] GROSS L R, PRUSSING J E. Optimal multiple-impulse direct ascent fixed-time rendezvous[J].AIAA Journal,1974, 12(7): 885-889.
[6] HUGHES S P, MAILHE L M, JJ Guzman. A comparison of trajectory optimization methods for the impulsive minimum fuel rendezvous problem [J].Advances in the Astronautical Sciences, 2003,11(3): 85-104.
[7] 王华,唐国金. 用遗传算法求解双冲量最优交会问题[J].中国空间科学与技术,2003(1): 26-30.
WANG H,TANG G J. Solving optimal rendezvous using two impulses based on genetic algorithms[J]. Chinese Space Science and Technology, 2003(1): 26-30. (in Chinese)
[8] KIM Y H, SPENCER D B. Optimal spacecraft rendezvous using genetic algorithms[J]. Journal of Spacecraft and Rockets, 2002,39(6): 859-865.
[9] ABDELKHALIK O, MORTARI D. Nimpluse orbittransfer using genetic algorithm[J]. Journal of Spacecraft and Rockets, 2007,44 (2): 456-460.
[10] 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 S, CHEN T,XU S J. Optimial 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)
[11] PONTANI M,GHOSH P,CONWAY B A. Particle swarm optimization of multiple-burn rendezvous trajectories[J]. Journal of Guidance Control and Dynamics, 2012,35(4),1192-1207.
[12] WEN C X, ZHAO Y S, LI B J, et al.. Solving the relative Lambert's problem and accounting for its singularities[J]. Acta Astronautica, 2014,97: 122-129.
[13] 张柏楠. 航天器交会对接任务分析与设计[M]. 北京: 科学出版社, 2011: 109-110,262-264.
ZHANG B N. Analysis and Design of Spacecraft Rendezvous and Docking Mission[M]. Beijing: Science Press, 2011: 109-110,262-264.(in Chinese)
[14] BESSETTE C R, SPENCER D B. Optimal space trajectory design: a heuristic-based approach[J]. Advances in Astronautical Sciences, 2006,6(124): 1611-1628.
[15] 陈全, 杨震, 罗亚中. 基于粒子群算法的多脉冲转移轨迹优化[J]. 空间控制技术与应用,2014,40(5): 25-30.
CHEN Q, YANG Z, LUO Y Z. Optimization of multi-impulse orbit transfer based on particle swarm optimization algorithm[J]. Aerospace Control and Application, 2014,40(5): 25-30.(in Chinese)
[16] PONTANI M,CONWAY B B. Optimal low-thrust orbital maneuvers via indirect swarming method[J]. Journal of Optimization Theory and Applications, 2014, 162(1): 272-292.
[17] SEDLACZECK K, EBERHARD R.Using augmented lagrangian particle swarm optimization for consrtrained problems in engineering[J] . Structural and Multidisciplinary Optimization , 2006,32(4): 277-286.
[18] HU X, EBERHART R. Solving constrained nonlinear optimization problems with particle swarm optimization[C]. Proceedings of the 6th World Multiconference on Systemics. Cybernetics and Informatics,2002.
[19] VENTER G, SOBIESZCZANSKI-SOBIESKI J. Particle swarm optimization [J]. AIAA Journal, 2003, 4(8): 1583-1589.
[20] ZHANG G, ZHOU D, MORTARI D. An approximate analytical method for short-range impulsive orbit rendezvous using relative Lambert solutions[J]. Acta Astronautica, 2012, 81(1): 318-324.
刘源, 叶潇, 郝勇, 李玉玲. 多脉冲异面交会对接转移轨道的优化[J]. 光学 精密工程, 2017, 25(4): 987. LIU Yuan, YE Xiao, HAO Yong, LI Yu-ling. Optimization of transfer orbit for multiple-pulse noncoplanar rendezvous and docking[J]. Optics and Precision Engineering, 2017, 25(4): 987.