[1]冯飞,张雅声.多约束条件下月球南极探测返回窗口设计[J].空间控制技术与应用,2017, 43(3):2127.
FENG F,ZHANG Y S.Design of Launch Window for Lunar South Pole Return Mission in MultiRestrictions[J].Aerospace Control and Application,2017,43(3):2127.
[2]CARPENTER J D,FISACKERLY R,DE ROSA D,et al.Scientific preparations for lunar exploration with the European Lunar Lander[J].Planetary and Space Science,2012, 74(1): 208223.
[3]Russian Federal Space Agency. Russia space programs and exploration handbook[R].Moscow: Russian Federal Space Agency, 2011: 59.
[4]BENJAMIN V, DIEGO DE R,RICHARD F,et al.An analysis of illumination and communication conditions near lunar south pole based on Kaguya data[C]//Proceedings of the 7th International Planetary Probe Workshop.Washington D. C.:NASA,2010:17.
[5]COLAPRETE A,SCHULTZ P,HELDMANN J,et al.Detection of water in the LCROSS ejecta plume[J].Science,2010, 330(6003):463468.
[6]WOODEN D H,COLAPRETE A,ENNICO K,et al.Lunar crater observation and sensing satellite (LCROSS) mission: results from the nadir nearinfrared spectrometer aboard the Shepherding spacecraft[J].Lunarand Planetary Institute Science Conference Abstracts.41, 2010:20252026.
[7]张锦绣,曹喜滨,张刘,等.J2项摄动下的Lambert问题算法研究[J].哈尔滨工业大学学报,2009(5):69.
ZHANG J X, CAO X B, ZHANG L, et al. An algorithm for Lambert solution based on J2 perturbation[J].Journal of Harbin Institute of Technology, 2009(5):69.
[8]HUANG W.Solving coplanar satellite rendezvous problem by primer vector approximation method[C]//AIAA/AAS Astrodynamic Specialist Conferences. Washington. D.C.: AIAA, 2012.
[9]徐明,谭田,李志武,等.Lambert 转移中途修正的全局概率最优策略[J].北京航空航天大学学报,2012, 38(5): 574578.
XU M, TAN T, LI Z W,et al.Optimal correction strategy during Lambert transfer from view of probability[J].Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(5): 574578.
[10]唐国金,罗亚中,雍恩米.航天器轨道优化理论、方法及应用[M].北京:科学出版社,2011.
TANG G J, LUO Y Z, YONG E M. Trajectory optimization theory, method and application[M].Beijing:Science Press,2012.
[11]FENG F, ZHANG Y S.Application and analysis of an improved multiconic method in trajectory design of the lunar south pole return mission[J].Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2017:0954410017705896.
[12]张磊,谢剑锋,刘勇.绕月返回飞行再入航程调整的轨道控制[J].飞行器测控学报, 2015,34(1):6469.
ZHANG L, XIE J F, LIU Y.Trajectory maneuver for reentry downrange modification during circumlunar return flight[J].Journal of Spacecraft TT&C Technology,2015,34(1):6469.
[13]LUO Y Z.Interactive optimization approach for optimal impulsive rendezvous using primer vector and evolutionary algorithms[J].ActaAstronautica,67(2):396405.
[14]罗亚中.空间最优交会路径规划策略研究 [D].长沙:国防科学技术大学,2007.
LUO Y Z.Study on Space Optimal Rendezvous Trajectory Planning Approach[D].Changsha:National University of Defense Technology, 2007.
[15]HANDELSMAN M,LION P M.Primer vector on fixedtime impulsive trajectories[J].AIAA Journal, 1968, 6(1): 127132.
[16]冯飞, 张雅声. 多约束条件下月球南极探测返回窗口设计[J].空间控制技术与应用, 2017, 43(3):2127.
FENG F, ZHANG Y S.Design of Launch Window for Lunar South Pole Return Mission with MultiRestrictions[J].Aerospace Control and Application,2017,43(3):2127. |