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

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

• We are an exchange download platform that only provides communication channels. The downloaded content comes from the internet. Except for download issues, please Google on your own.
• The downloaded content is provided for members to upload. If it unintentionally infringes on your copyright, please contact us.
• Please use Winrar for decompression tools
• If download fail, Try it againg or Feedback to us.
• If downloaded content did not match the introduction, Feedback to us，Confirm and will be refund.
• Before downloading, you can inquire through the uploaded person information

Nothing．