High accuracy coning compensate algorithm by angular velocity

[1] Miller R B.A new strap-down attitude algorithm[J].Journal of Guidance Control and Dynamics,1983,6(4):287~291 [2] Jiang Y F,Lin Y P.Improved strap-down coning algorithms[J].IEEE Transaction on Arospace and Electronic System,1992,28(2):484~490 [3] 刘 危,解旭辉,李圣怡.捷联惯导系统的圆锥误差补偿算法研究[J].南京航空航天大学学报,2004,36(3):348~352 Liu Wei,Xie Xuhui,Li Shengyi.Coning algorithm for strapdown inertial navigation system[J].Journal of Nanjing University of Aeronautics & Astronautics, 2004,36(3):348~352(in Chinese) [4] 缪玲娟,林 丽.减小动态误差的捷联系统姿态算法研究[J].兵工学报,2000,21(3):229~232 Miao Lingjuan,Lin Li.Research on strapdown attitude algorithm for decreasing dynamic error[J].Journal of Binggong,2000,21(3):229~232(in Chinese) [5] 黄 昊.光纤陀螺捷联姿态算法及应用研究. 哈尔滨:哈尔滨工业大学控制工程系,2001 Huang Hao.Research on the fiber optic gyroscope strapdown attitude algorithm and application. Harbin:Department of Control Enginerring,　Harbin Institute of Technology, 2001(in Chinese) [6] 黄 昊,邓正隆.旋转矢量航姿算法的一种新的表达式[J].宇航学报,2001,22(3):92~98 Huang Hao, Deng Zhenglong.A new expression of rotation vector for navigation attitude algorithm[J].Journal of space navigation, 2001,22(3):92~98(in Chinese) [7] 杨艳娟.捷联惯导系统关键技术研究. 哈尔滨:哈尔滨工业大学自动化学院,2001 Yang Yanjuan.Research on the key technology of strapdown inertial navigation system. Harbin:Automation School,University of Harbin Institute of Technology, 2001(in Chinese)