[1] Lahham J I, Wigent D J, Coleman A L. Tuned support structure for structure-borne noise reduction of inertial navigator with dithered ring laser gyros (RLG)[C]∥Proceedings of IEEE Position Location and Navigation Symposium. San Diego, CA, US: IEEE,2000: 419-428. [2] 袁保伦. 四频激光陀螺旋转式导航系统研究[D]. 长沙:国防科学技术大学,2007:71-80. YUAN Bao-lun. Research on rotating inertial navigation system with four-frequency differential laser gyroscope[D]. Changsha: National University of Defense Technology, 2008:71-80. (in Chinese) [3] Titterton D H, Weston J L. Strapdown inertial navigation technology[M]. Stevenage, Hertfordshire, UK: Institution of Electrical Engineers, 2004. [4] 严恭敏. 捷联惯导系统动基座初始对准及其它相关问题研究 [R]. 西安:西北工业大学, 2008. YAN Gong-min. On SINS in-movement initial alignment and some other problems[R]. Xi'an: Northwestern Polytechnical University, 2008. (in Chinese) [5] Hong S, Lee M H, Chun H, et al. Experimental study on the estimation of lever arm in GPS/INS[J]. IEEE Transactions on Vehicular Technology, 2006, 55(2): 431-448. [6] 严恭敏,严卫生,徐德民. 捷联惯性测量组件中内杆臂效应分析与补偿[J]. 中国惯性技术学报, 2008, 16(2):148-153. YAN Gong-min, YAN Wei-sheng, XU De-min. Analysis and compensation on inner lever arm effect of strapdown inertial measurement unit[J]. Journal of Chinese Inertial Technology, 2008, 16(2): 148-153.(in Chinese) [7] 周冉辉. 舰用高精度激光陀螺惯导内杆臂误差分析及补偿方法研究[J]. 舰船科学技术, 2016, 38(4):120-123. ZHOU Ran-hui. Rotating scheme designing for two-axis rotating laser gyro inertial navigation system[J]. Ship Science and Technology, 2016, 38(4): 120-123. (in Chinese) [8] 梁茂柱, 王超, 杜鹏程. 单轴旋转引起加速度计尺寸效应误差分析及补偿[J]. 弹箭与制导学报, 2013, 33(1):179-181. LIANG Mao-zhu, WANG Chao, DU Peng-cheng. Compensation and analysis on size effect error of accelerometers of INS caused by single-axial rotation[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013, 33(1): 179-181. (in Chinese) [9] 吴文启, 杨伟光, 杨杰. 激光陀螺捷联惯导系统尺寸效应参数标定与优化补偿[J]. 中国惯性技术学报, 2009, 17(6):636-642. WU Wen-qi, YANG Wei-guang, YANG Jie. Calibration and optimal compensation for size effect parameters of laser gyro SINS[J]. Journal of Chinese Inertial Technology, 2009, 17(6): 636-642. (in Chinese) [10] 严恭敏, 周琪, 翁浚, 等. 捷联惯导系统内杆臂补偿方法及试验[J]. 宇航学报, 2012, 33(1):62-67. YAN Gong-min, ZHOU Qi, WENG Jun,et al. Inner lever arm compensation and its test verification for SINS[J]. Journal of Astronautics, 2012, 33(1): 62-67. (in Chinese) [11] 王立冬, 蔡玲. 车载捷联惯导系统静止条件下的初始对准方法研究[J]. 中国惯性技术学报, 2004, 12(2):1-5. WANG Li-dong, CAI Ling. Initial alignment method of SINS in stationary state[J]. Journal of Chinese Inertial Technology, 2004, 12(2): 1-5. (in Chinese) [12] 秦永元. 惯性导航[M]. 北京:科学出版社, 2006: 35-37. QIN Yong-yuan. Inertial navigation[M]. Beijing: Science Press, 2006: 35-37. (in Chinese) [13] 刘准, 陈哲. 条件数在系统可观测性分析中的应用研究[J]. 系统仿真学报, 2004, 16(7):1552-1555. LIU Zhun, CHEN Zhe. Application of condition number in analysis observability of system[J]. Journal of System Simulation, 2004, 16(7): 1552-1555. (in Chinese)
第38卷 第7期2017 年7月兵工学报ACTA ARMAMENTARIIVol.38No.7Jul.2017
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