ahrs.UKF.QUATERNION: Estimate the current quaternion attitude by UKF-based AHRS...

Description Usage Arguments Value Author(s) References

Description

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.

Usage

1
ahrs.UKF.QUATERNION(Filter, Sensors, Parameters)

Arguments

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

Value

data structure for Unscented Kalman Filter

Author(s)

Jose Gama

References

Vlad Maximov, 2012 Scalar Calibration of Vector accelerometers and magnetometers, GyroLib documentation


RAHRS documentation built on May 2, 2019, 2:42 a.m.