LEVINSON E, MAJURE R. Accuracy enhancement techniques applied to the marine ring laser inertial navigation [J]. Journal of the Institute of Navigation, 1987,34(1):64-86.
[2]
孙枫,孙伟,郭真.基于IMU旋转的捷联惯导系统自补偿方法[J].仪器仪表学报,2009,30(12):2511-2517.SUN Feng, SUN Wei, GUO Zhen. Auto-compensation method of SINS based on IMU rotation [J]. Chinese Journal of Scientific Instrument, 2009,30(12):2511-2517.
[3]
LAHHAM J I, BRAZELL J R. Acoustic noise reduction in the MK49 ships inertial navigation system[C]//IEEE Position Location and Navigation Symposium. Monterey,USA,1992:32-39.
[4]
LEVINSON E, WILLCOCKS M. The next marine inertial navigation is here now[C]//IEEE Position Location and Navigation Symposium. Las Vegas,USA,1994: 121-127.
[5]
郝燕玲,张义,孙枫.单轴旋转式捷联惯导方位对准研究[J].仪器仪表学报,2011,32(2): 309-315.HAO Yanling, ZHANG Yi, SUN Feng. Analysis of single-axial rotation SINS azimuth alignment [J]. Chinese Journal of Scientific Instrument, 2011,32(2): 309-315.
[6]
汪滔,吴文启,曹聚亮.基于转动的管线陀螺捷联系统初始对准研究[J].压电与声光,2007,29(5):519-522.WANG Tao, WU Wenqi, CAO Juliang. Study on initial alignment of fiber optic gyro SINS based on rotation [J]. Piezoelectectrics & Acoustooptics, 2007,29(5):519-522.
[7]
李瑶,徐晓苏,吴炳祥.捷联惯导系统罗经法自对准[J].中国惯性技术学报,2008,16(4):386-389.LI Yao, XU Xiaosu, WU Bingxiang. Gyrocompass self-alignment of SINS [J]. Journal of Chinese Inertial Technology, 2008,16(4):386-389.
[8]
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: 7-9.WAN Dejun, FANG Jiancheng. Initial alignment of inertial navigation [M].Nanjing: Southeast University Press, 1998: 7-9.
[9]
GOSHEN-MESHIN D, BAR-ITZHACK I Y. Observability analysis of piece-of wise constant system, part I: theory [J]. IEEE Transactions on Aerospace and Eleectronic Systems, 1992, 28(4):1056-1067.
[10]
GOSHEN-MESHIN, BAR-ITZHACK I Y. Observability analysis of piece-of wise constant system, part II: application to inertial navigation in-flight alignment[J]. IEEE Transactions on Aerospace and Electronic Systems, 1992, 28(4):1068-1075.
[11]
FANG J G, WANG D J. A fast initial alignment method for strapdown inertial navigation system on stationary base [J]. IEEE Transactions on Aerospace and Electronic Systems, 1996, 32(4): 1501-1505.
[12]
金翔,王大海. 光纤陀螺捷联系统最优多位置对准[J]. 中国惯性技术学报,2003,11(4): 9-13.JIN Xiang, WANG Dahai. Multiposition alignment of fiber optic gyro strapdown inertial navigation system [J]. Journal of Chinese Inertial Technology, 2003,11(4): 9-13.
[13]
刘志琴,王新龙. 捷联惯导系统最优多位置对准的确定与分析[J]. 北京航空航天大学学报,2013,39(3): 330-334.LIU Zhiqing, WANG Xinglong. Confirmation and analysis on the optimal multiposition alignment of strapdown inertial navigation system [J]. Journal of Beijing University of Aeronautics and Astronautics, 2013,39(3): 330-334.
[14]
孙枫,孙伟. 旋转捷联惯导系统精对准技术[J].系统工程与电子技术,2010,32(3):630-633,659.SUN Feng, SUN Wei. Fine alignment by rotation in strapdown inertial navigation systems [J]. System Engineering and Electronics, 2010,32(3):630-633,659.
[15]
JIANG Y F, LIN Y P. Error estimation of INS ground alignment through observability analysis [J]. IEEE Transaction on Aerospace and Electronic Systems, 1992,28(1):92-97.
[16]
徐晓苏,孙学慧,扶文树. 弹载捷联惯导系统快速两位置对准 [J].中国惯性技术学报,2007,15(2):139-142.XU Xiaosu, SUN Xuehui, FU Wenshu. Fast two-position self-alignment in missile SINS [J]. Journal of Chinese Inertial Technology, 2007,15 (2):139-142.
[17]
杨艳娟,卞鸿巍,田蔚风. 一种新的INS/GPS组合导航技术[J].中国惯性技术学报,2004,12(2):23-26,35.YANG Yanjuan, BIAN Hongwei,TIAN Weifeng. A new INS/GPS integrated navigation technique[J]. Journal of Chinese Inertial Technology, 2004,12 (2):23-26,35.