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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- [clear] - The original code, including procedures
- [IMU] - Based on onboard IMU/C: PS Integrated Na
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激光陀螺随机漂移数据的非参数建模.kdh
激光陀螺随机误差建模方法研究.caj
激光陀螺误差模型研究.nh
AttitudeAlgorithmwithIncrementalAngleofRLGSINS.pdf
激光陀螺随机漂移的数字滤波方法比较.caj
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