GNSS/Odometer/IMU integrated navigation system based on error state Kalman Filter
This project implements a simplified GNSS/Odometer/IMU integrated navigation system with error state Kalman Filter. Three types of data: GNSS, Odometry and IMU are used for the sensor fusion. The error state Kalman Filter is used to estimate the state of the system which includes position, rotation, velocity, bias of accerometer, bias of gyroscope and gravity.