• Attitude Estimation based on Extended Kalman Filtering method. • Gyro bias estimation to improve the robustness of the algorithm. • Attitude prediction to be done using gyro output. • Attitude is updated using accelerometer and magnetometer output.
c
quadcopter
cplusplus
cpp
filter
magnetometer
ekf
bias
kalman
ahrs
heading
estimation-algorithm
accelerotmeter
-
Updated
May 8, 2020