Brady T,Paschall S,Crain T P.GN&C development for future lunar landing missions [C]//AIAA Guidance,Navigation,and Control Conference.Toronto:AIAA,2010
[2]
Biegler L T.An overview of simultaneous strategies for dynamic optimization[J].Chemical Engineering and Processing:Process Intensification,2007,46(11):1043-1053
[3]
王大轶,李铁寿,马兴瑞.月球最优软着陆两点边值问题的数值解法[J].航天控制,2000,3:44-49 Wang Dayi,Li Tieshou,Ma Xingrui.Numerical solution of TPBVP in optimal lunar soft landing[J].Aerospace Control,2000,3:44-49(in Chinese)
[4]
赵吉松,谷良贤,潘雷.月球最优软着陆两点边值问题的数值解法[J].中国空间科学技术,2009,4:21-27 Zhao Jisong,Gu Liangxian,Pan Lei.Numerical solution of TPBVP for optimal lunar soft landing[J].Chinese Space Science and Technology,2009,4:21-27(in Chinese)
[5]
Sostaric R R.Powered descent trajectory guidance and some considerations for human lunar landing [C]//AAS 30th Annual AAS Guidance and Control Conference.Colorado:AAS,2007
[6]
Lee A Y.Fuel-efficient descent and landing guidance logic for a safe lunar touchdown [C]//AIAA Guidance,Navigation,and Control Conference.Portland:AIAA,2011
[7]
Yan Hui,Wu Hongxin.Initial adjoint variable guess technique and its application in optimal orbital transfer [R].AIAA-98-4551,1998
