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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激光陀螺滤波评估方法研究.caj
激光陀螺滤波评估方法研究.pdf
激光陀螺漂移数据的自适应Kalman滤波.caj
激光陀螺漂移数据建模及分析.kdh
激光陀螺捷联姿态测量系统误差建模与仿真研究.pdf
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