Vasile M,Minisci E,Locatelli M.On testing global optimization algorithms for space trajectory design [R].AIAA2008-6277,2008
[2]
Vasile M,Pascale P De.Preliminary design of multiple gravity-assist trajectories[J].Journal of Spacecraft and Rockets,2006,43(4):794-805
[3]
Addis B,Cassioli A,Locatelli M,et al.A global optimization method for the design of space trajectories[J].Computational Optimization and Applications,2011,48(3):635-652
[4]
Zhu K J,Li J F,Baoyin H X.Multi-swingby optimization of mission to Saturn using global optimization algorithms[J].Acta Mechanica Sinica,2009,25(6):839-845
[5]
Izzo D,Becerra V M,Myattet D R,et al.Search space pruning and global optimisation of multiple gravity assist spacecraft trajectories[J].Journal of Global Optimization,2007,38(2):283-296
[6]
马文臻.深空探测器的轨道设计与优化 [D].北京:中国科学院研究生院,2006 Ma Wenzhen.Trajectory design and optimization for deep space exploration probe [D].Beijing:Graduate University of Chinese Academy of Sciences,2006(in Chinese)
[7]
Strange N J,Sims J A.Methods for the design of V-infinity leveraging maneuvers [C]//Spencer D B.AAS,Astrodynamics 2001,Pts I-Iii.San Diego:Univelt Inc,2001:1959-1976
[8]
Kloster K W,Petropoulos A E,Longuski J M.Europa orbiter tour design with Io gravity assists[J].Acta Astronautica,2011,68(7-8):931-946
[9]
Strange N,Russell R,Buffington B.Mapping the v-infinity globe [C]//Proulx R J.AAS,Astrodynamics.2007,129 Pts I-Iii.San Diego:Univelt Inc,2008:423-446
[10]
Strange N,Spilker T L,Landau D F,et al.Mission design for the Titian Saturn system mission concept [C]//AV Rao.AAS,Astrodynamics 2009.San Dieg:Univelt Inc,2008:919-934
[11]
马文臻,郑建华,高长生.太阳高纬探测器的借力飞行轨道设计[J].北京航空航天大学学报,2006,32(8):917-921 Ma Wenzhen,Zheng Jianhua,Gao Changsheng.Trajectories to the far side of the sun via gravity assists [J].Journal of Beijing University of Aeronautics and Astronautics,2006,32(8):917-921(in Chinese)
