Description Usage Arguments Value Author(s) References
Estimates the current quaternion attitude with an implementation of the UKF-based AHRS algorithm based on measurements from three-component accelerometer with orthogonal axes, vector magnetometer and three-axis gyroscope.
1 | ahrs.UKF.QUATERNION(Filter, Sensors, Parameters)
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Filter |
data structure for Unscented 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 |
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 |
data structure for Unscented Kalman Filter
Jose Gama
Vlad Maximov, 2012 Scalar Calibration of Vector accelerometers and magnetometers, GyroLib documentation
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