Description: Based on onboard IMU/C: PS Integrated Navigation System Alignment conducted a study and simulation first analyzed onboard IMU and GI S of the system error, the establishment of the system error model obtained and then, using Kalman filter technology, designed Missile IMU/UPS Integrated Navigation System Alignment Algorithm
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激光陀螺捷联惯导系统元件误差自标定技术.caj
激光陀螺捷联惯导系统中整周期采样的修正研究.caj
激光陀螺捷联惯导系统中整周期采样的修正研究.pdf
激光陀螺捷联惯性导航系统的误差参数标定.pdf
激光陀螺惯导系统硬件增强角速率输入圆锥算法.pdf
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