[1] 李杰,赵诣,刘俊,等.高旋弹药飞行姿态测量用半捷联 MEMS 惯性测量装置研究[J].兵工学报,2013,34(11): 1398-1403. LI Jie, ZHAO Yi, LIU Jun,et al. Research on semi-strapdown MEMS inertial measurement device for flight attitude measurement of high-speed rotating ammunition[J].Acta Armamentarii, 2013,34(11): 1398-1403.(in Chinese) [2] 鲍 亚琪,陈国光,吴坤,等.基于磁强计和MEMS陀螺的弹箭全姿态 探测[J].兵工学报,2008,29(10): 1227-1231. BAO Ya-qi, CHEN Guo-guang, WU Kun,et al.Research on attitude determination using magnetometers and MEMS inertial sensors[J]. Acta Armamentarii, 2008,29(10): 1227-1231.(in Chinese) [3] 中 北大学.一种适用于高旋弹药的主动式半捷联惯性测量装置: 中国,201110025530 [P].2011-08-17. North University of China. One for the high-spin ammunition semi-active strapdown inertial measurement unit: China, 201110025530 [P].2011-08-17.(in Chinese) [4] 高峰,张合.基于基准角和补偿角的常规弹药滚转角磁探测算法研究[J]. 探测与控制学报,2008,30(5): 11-15. GAO Feng, ZHANG He. Algorithm of roll angle determination of conventional ammunitions based on benchmark angle and compensation angle[J]. Journal of Detection & Control, 2008,30(5): 11-15.(in Chinese) [5] 赵 岩,程烘炳,吴训忠,等.基于MEMS的低成本 SINS/GPS 组合 导航系统研究[J].传感器与微系统,2011,30(8): 18-21. ZHAO Yan, CHENG Hong-bing, WU Xun-zhong, et al. Study on low cost SINS/GPS integrated navigation system based on MEMS[J]. Transducer and Microsystem Technologies, 2011,30(8): 18-21.(in Chinese) [6] 张松,李杰,赵诣,等.半捷联 MEMS 惯性测量装置数据硬回收系统设计[J].传感技术学报,2013,26(9): 1219-1223. ZHANG Song, LI Jie, ZHAO Yi,et al. Design of acquisition and storage system on half-strapdown system[J].Chinese Journal of Sensors and Actuators, 2013,26(9): 1219-1223.(in Chinese) [7] 蒋 巍巍.基于MEMS 的导航系统的初始对准及其相关问题研究[D]. 沈阳:沈阳理工大学, 2013. JIANG Wei-wei. Based on MEMS research on initial alignment in navigation system and its associated problems[D]. Shenyang : Shenyang Ligong University, 2013.(in Chinese) [8] 梁 勇.基于MEMS 的航姿系统的设计与实现[D].哈尔滨:哈尔滨 工程大学,2011. LIANG Yong. The design and implementation of navigation posture system based on the MEMS[D]. Harbin:Harbin Engineering University, 2011.(in Chinese) [9] 牛 春峰,刘世平,王中原.制导炮弹飞行姿态的卡尔曼滤波估计 方法[J].中国惯性技术学报, 2012, 20(5): 510-514. NIU Chun-feng, LIU Shi-ping, WANG Zhong-yuan. Approach of Kalman filtering estimation of guided projectile attitude[J]. Journal of Chinese Inertial Technology, 2012, 20(5): 510-514.(in Chinese) [10] 程 向红,黄华.捷联惯性系统初始对准中IMU安装误差及陀螺 漂移的估计与补偿[J].中国惯性技术学报,2005, 12(5): 13-15. CHENG Xiang-hong, HUANG Hua. Estimatin and compensation of IMU misalignment and gyros drifts during SINS initial alignment[J]. Journal of Chinese Inertial Technology, 2005, 12(5): 13-15.(in Chinese) [11] 赵长山,秦永元,夏家和.车载惯导里程仪组合导航系统安装误差标定研究[J].计算机测量与控制,2008,16(10): 1393-1395. ZHAO Chang-shan, QIN Yong-yuan, XIA Jia-he. On SINS installation error of a multimode vehicular navigation system[J]. Computer Measurement & Control, 2008,16(10): 1393-1395.(in Chinese) |