Description Usage Arguments Value Author(s) References
Attitude quaternion estimation by means of complementary Kalman filter.
1 | ahrs.LKF.VMATCH(Filter, Sensors, q, Parameters)
|
Filter |
data structure for Linear Kalman Filter Filter.x State vector [3x1] Filter.P Covariance matrix [3x3] Filter.Q System noise matrix [3x3] Filter.R Measurement noise matrix [6x6] |
Sensors |
sensors data structure Sensors.w current calibrated gyroscope measurement [3x1], rad/sec Sensors.a current calibrated accelerometer measurement [3x1], g Sensors.m current calibrated magnetometer measurement [3x1], |m| = 1 |
q |
quaternion |
Parameters |
AHRS Parameters Parameters.mn Magnetic Field Vector In Navigation Frame [3x1], |m| = 1 Parameters.an Acceleration vector In Navigation Frame [3x1], g Parameters.dt Sampling period, 1/Hz |
Filter |
data structure for Linear Kalman Filter |
Q |
Correct quaternion |
Jose Gama
Vlad Maximov, 2012 Scalar Calibration of Vector accelerometers and magnetometers, GyroLib documentation
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