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EKF: Add function to reset yaw and magnetic field states

master
Paul Riseborough 9 years ago committed by Roman
parent
commit
6140d4b21f
  1. 6
      EKF/ekf.h
  2. 30
      EKF/ekf_helper.cpp

6
EKF/ekf.h

@ -128,6 +128,8 @@ private: @@ -128,6 +128,8 @@ private:
float _mag_innov_var[3]; // earth magnetic field innovation variance
float _heading_innov_var; // heading measurement innovation variance
float _mag_declination = 0.0f; // magnetic declination used by reset and fusion functions (rad)
// complementary filter states
Vector3f _delta_angle_corr; // delta angle correction vector
Vector3f _delta_vel_corr; // delta velocity correction vector
@ -195,6 +197,10 @@ private: @@ -195,6 +197,10 @@ private:
// reset velocity states of the ekf
void resetVelocity();
// reset the heading and magnetic field states using the declination and magnetometer measurements
// return true if successful
bool resetMagHeading(Vector3f &mag_init);
// reset position states of the ekf (only vertical position)
void resetPosition();

30
EKF/ekf_helper.cpp

@ -94,6 +94,36 @@ void Ekf::resetHeight() @@ -94,6 +94,36 @@ void Ekf::resetHeight()
}
}
// Reset heading and magnetic field states
bool Ekf::resetMagHeading(Vector3f &mag_init)
{
// If we don't a tilt estimate then we cannot initialise the yaw
if (!_control_status.flags.tilt_align) {
return false;
}
// get the roll, pitch, yaw estimates and set the yaw to zero
matrix::Quaternion<float> q(_state.quat_nominal(0), _state.quat_nominal(1), _state.quat_nominal(2),
_state.quat_nominal(3));
matrix::Euler<float> euler_init(q);
euler_init(2) = 0.0f;
// rotate the magnetometer measurements into earth axes
matrix::Dcm<float> R_to_earth_zeroyaw(euler_init);
Vector3f mag_ef_zeroyaw = R_to_earth_zeroyaw * mag_init;
euler_init(2) = _mag_declination - atan2f(mag_ef_zeroyaw(1), mag_ef_zeroyaw(0));
// calculate initial quaternion states
_state.quat_nominal = Quaternion(euler_init);
_output_new.quat_nominal = _state.quat_nominal;
// calculate initial earth magnetic field states
matrix::Dcm<float> R_to_earth(euler_init);
_state.mag_I = R_to_earth * mag_init;
return true;
}
// This function forces the covariance matrix to be symmetric
void Ekf::makeSymmetrical()
{

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