空空导弹动基座对准长时间空中修正方法
[1] KAIN J E, CLOUTIER J R. Rapid transfer alignment for tactical weapon applications[C]//AIAA, 1989: 3581-3587.
[2] 王力丹, 张洪钺, 戴汝为.一种快速传递对准的方法[J]. 航天控制, 2000(4): 8-16. (WANG L D, ZHANG H Y, DAI R W. A method for rapid transfer alignment[J]. Aerospace Control, 2000(4): 8-16. )
[3] 夏家和. 舰载机惯导系统的动基座对准技术研究[D]. 西安:西北工业大学, 2007:52-56. (XIA J H. The research of transfer alignment for shipboard plane INS[D]. Xi'an:Northwestern Polytechnical University, 2007:52-56. )
[4] MOCHALOV A C, KAZANTSEV A V. Use of the ring laser units for measurement of the moving object deformation[C]//Proceedings of SPIE, 2002, 4680: 85-92.
[5] 王司, 邓正隆. 惯导系统动基座传递对准技术综述[J]. 中国惯性技术学报, 2003, 11(2): 61-67. (WANG S, DENG Z L. Technique review of transfer alignment for inertial navigation system on moving base[J]. Journal of Chinese Inertial Technology, 2003, 11(2): 61-67. )
[6] 鲁浩, 杜毅民, 王纪南. 应用于近距空空导弹惯导系统的传递对准技术[J]. 中国惯性技术学报, 2005, 10(5): 10-15. (LU H, DU Y M, WANG J N. Transfer alignment technology for INS of AAM[J]. Journal of Chinese Inertial Technology, 2005, 10(5): 10-15. )
[7] 万德钧, 房建成. 惯性导航初始对准[M]. 南京: 东南大学出版社, 1998: 69-72. (WAN D J, FANG J C. Initial alignment of inertial navigation[M]. Nanjing: Southeast University Press, 1998: 69-72. )
[8] 秦永元. 惯性导航[M]. 北京:科学出版社, 2006:355-361. (QING Y Y. Inertial navigation[M]. Beijing: Science Press, 2006: 355-361. )
[9] 袁信, 俞济祥, 陈哲. 导航系统[M]. 北京:航空工业出版社, 1993: 40-41. (YUAN X, YU J X, CHEN Z. Navigation system[M]. Beijing:Aviation Industry Press, 1993: 40-41. )
刘伟鹏, 张迪, 宋振华, 江振. 空空导弹动基座对准长时间空中修正方法[J]. 电光与控制, 2016, 23(2): 83. LIU Wei-peng, ZHANG Di, SONG Zhen-hua, JIANG Zhen. Long-Time Rectification in Flight for Transfer Alignment of AAMs[J]. Electronics Optics & Control, 2016, 23(2): 83.