College of Optoelectronic Science and Engineering, National University of Defense Technology, Changsha, China;
College of Optoelectronic Science and Engineering, National University of Defense Technology, Changsha, China;
College of Optoelectronic Science and Engineering, National University of Defense Technology, Changsha, China;
College of Optoelectronic Science and Engineering, National University of Defense Technology, Changsha, China;
College of Optoelectronic Science and Engineering, National University of Defense Technology, Changsha, China;
College of Optoelectronic Science and Engineering, National University of Defense Technology, Changsha, China;
Inertial Navigation; Systematic calibration; Kalman filter; Error separation;
机译:环形激光陀螺惯性导航系统的误差建模,标定和非线性插值补偿方法
机译:环形激光陀螺惯性导航系统的误差建模,标定和非线性插值补偿方法
机译:无陀螺捷联惯性导航系统的导航应用及标定方法
机译:环形激光陀螺惯用导航系统的新系统校准方法
机译:一种机载重力惯性稳定平台中陀螺仪的现场校准方法。
机译:双轴旋转惯性导航系统中安装错误的系统级自校准方法
机译:中等级惯性导航小环激光陀螺设计要求的研究
机译:捷联环形激光陀螺四分体惯性导航系统的飞行试验结果