[1] 武庆雅. 旋转弹药的惯性导航与解耦控制方法研究[D]. 北京:北京理工大学, 2015. WU Q Y. Research on inertial navigation and decoupling control method for spinning ammunition [D].Beijing: Beijing Institute of Technology, 2015.(in Chinese) [2] 苗劲松, 翟英存, 苟秋雄, 等. 基于卫星/地磁组合的弹箭滚转姿态解算方法[J]. 弹箭与制导学报, 2014,34(5):63-66. MIAO J S, ZHAI Y C, GOU Q X, et al. Solving method for roll attitude of rocket based on global navigation satellite system/magnetic sensor[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014,34(5):63-66.(in Chinese) [3] 闫爱天. 基于地磁传感器与MEMS陀螺仪组合姿态测量技术研究[D]. 南京:南京理工大学, 2016. YAN A T. Research on combined attitude measurement technology based on geomagnetic sensor and MEMS gyroscope[D]. Nanjing: Nanjing University of Science and Technology, 2016.(in Chinese) [4] 田利伟, 陈国光, 孙汉琴, 等. 弹箭滚转姿态地磁测角仪的卡尔曼滤波算法[J]. 弹箭与制导学报, 2017, 37(1):139-143. TIAN L W, CHEN G G, SUN H Q, et al.Kalman filtering algorithm of projectile rolling attitude geomagnetic goniometer[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2017,37(1): 139-143.(in Chinese) [5] 李兴隆, 姚文进, 朱立坤, 等. 捷联激光探测器组合GPS测量弹丸滚转角方法[J]. 兵工学报, 2016, 37(2):279-286. LI X L, YAO W J, ZHU L K, et al.Projectile roll angle measurement method of a combination ofstrapdown laser detector and GPS measurement for semi-active laser terminal correction[J]. Acta Armamentarii, 2016,37(2):279-286.(in Chinese) [6] 佘浩平, 杨树兴, 倪慧. GPS/INS组合制导弹药空中对准的初始滚转角估计新算法[J]. 兵工学报, 2011,32(10):1265-1270. SHE H P, YANG S X, NI H. New algorithms to estimate initial roll angle for in-flight alignment of GPS/INS guided munitions[J]. Acta Armamentarii, 2011,32(10):1265-1270.(in Chinese) [7] WU Y X, PAN X F. Velocity/position integration formula (Ⅰ): application to in-flight coarse alignment[J]. IEEE Transactions on Aerospace and Electronic Systems, 2012,49(2):1006-1023. [8] WU Y X, PAN X F. Velocity/position integration formula(III): application to strapdown inertial navigation computation[J]. IEEE Transactions on Aerospace and Electronic Systems, 2013,49(2):1024-1034. [9] 杨登红. 旋转稳定弹GNSS/MIMU组合导航初始对准方法研究[D]. 北京:北京理工大学, 2015. YANG D H. Research on initial alignment method of GNSS/IMU integrated navigation for spin-stabilized projectile[D]. Beijing: Beijing Institute of Technology, 2015.(in Chinese)
[10] 杨莉. 基于GPS/SINS组合导航算法的优化设计与仿真[D]. 北京:中国科学院大学, 2015. YANG L. Optimization design and simulation of integrated navigation algorithm based on GPS/SINS[D]. Beijing: University of Chinese Academy of Sciences, 2015.(in Chinese) [11] NOURELDIN A, KARAMAT T B, GEORGY J. Fundamentals of inertial navigation, satellite-based positioning and their integration[M]. Heidelberg, Baden-Württemberg, Germany: Springer-Verlag Berlin Heidelberg, 2013. [12] HU X M, LIU F, WENG H N. Observability analysis of MSINS/GPS complete integrated system [J]. Journal of Chinese Inertial Technology, 2011,19(1):38-45. [13] 董进龙, 莫波. 典型弹道下的火箭弹MEMS-INS/GNSS组合导航姿态误差可观性分析[J]. 兵工学报, 2014,35(6):850-856. DONG J L, MO B. Observerbility analysis of rocket MEMS-INS/GNSS integrated navigation system attitude in classic trajectories [J]. Acta Armamentarii, 2014,35(6):850-856.(in Chinese) [14] 孔星炜, 董景新, 吉庆昌, 等. 一种基于PWCS的惯导系统可观测度分析方法[J]. 中国惯性技术学报, 2011,19(6):631-636. KONG X W, DONG J X, JI Q C, et al. INS observable degree analysis method based on PWCS [J]. Journal of Chinese Inertial Technology, 2011,19(6):631-636.(in Chinese) [15] HONG S, MAN H L, RIOS J A, et al. Observability analysis of INS with a GPS multi-antenna system[J]. KSME International Journal, 2002,16(11):1367-1378. [16] RHEE I, ABDEL-HAFEZ M F, SPEYER J L. Observability of an integrated GPS/INS during maneuvers[J]. IEEE Transactions on Aerospace and Electronic Systems, 2004, 40(2):526- 535.
第40卷 第7期2019 年7月兵工学报ACTA ARMAMENTARIIVol.40No.7Jul.2019
|