Description: using quaternion approach derived platform SDINS mathematical equations and the error rate of error equation, and the establishment of this initial alignment error nonlinear model, extended Kalman Filter (EKF) for precision alignment, EASY determine the initial angle.
- [KF_SINS] - this is my preparation access inertial n
- [KF_SINS_modify2] - using MATLAB access Inertial Navigation
- [gps_matlab] - MATLAB programming format of the GPS dat
- [clear] - The original code, including procedures
- [dhjs] - An inertial navigation solution counting
- [ins] - I have written the application of robust
- [ekf_pf] - Based on the Kalman filter and particle
- [conicalmotion] - Quaternion method using the standard con
- [Geometric] - Image geometric transformation, such as
File list (Check if you may need any files):
Download