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enable estimator state and innovations data logging

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Roman
2016-01-22 11:31:14 +01:00
committed by Roman Bapst
parent 86df68e404
commit 8d0022ab1e
6 changed files with 446 additions and 164 deletions
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EKF/vel_pos_fusion.cpp
+8 -8
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@@ -44,29 +44,28 @@
void Ekf::fuseVelPosHeight()
{
bool fuse_map[6] = {};
float innovations[6] = {};
float R[6] = {};
float Kfusion[24] = {};
// calculate innovations
if (_fuse_hor_vel) {
fuse_map[0] = fuse_map[1] = true;
innovations[0] = _state.vel(0) - _gps_sample_delayed.vel(0);
innovations[1] = _state.vel(1) - _gps_sample_delayed.vel(1);
_vel_pos_innov[0] = _state.vel(0) - _gps_sample_delayed.vel(0);
_vel_pos_innov[1] = _state.vel(1) - _gps_sample_delayed.vel(1);
R[0] = _params.gps_vel_noise;
R[1] = _params.gps_vel_noise;
}
if (_fuse_vert_vel) {
fuse_map[2] = true;
innovations[2] = _state.vel(2) - _gps_sample_delayed.vel(2);
_vel_pos_innov[2] = _state.vel(2) - _gps_sample_delayed.vel(2);
R[2] = _params.gps_vel_noise;
}
if (_fuse_pos) {
fuse_map[3] = fuse_map[4] = true;
innovations[3] = _state.pos(0) - _gps_sample_delayed.pos(0);
innovations[4] = _state.pos(1) - _gps_sample_delayed.pos(1);
_vel_pos_innov[3] = _state.pos(0) - _gps_sample_delayed.pos(0);
_vel_pos_innov[4] = _state.pos(1) - _gps_sample_delayed.pos(1);
R[3] = _params.gps_pos_noise;
R[4] = _params.gps_pos_noise;
@@ -74,7 +73,7 @@ void Ekf::fuseVelPosHeight()
if (_fuse_height) {
fuse_map[5] = true;
innovations[5] = _state.pos(2) - (-_baro_sample_delayed.hgt); // baro measurement has inversed z axis
_vel_pos_innov[5] = _state.pos(2) - (-_baro_sample_delayed.hgt); // baro measurement has inversed z axis
R[5] = _params.baro_noise;
}
@@ -89,6 +88,7 @@ void Ekf::fuseVelPosHeight()
// compute the innovation variance SK = HPH + R
float S = P[state_index][state_index] + R[obs_index];
_vel_pos_innov_var[obs_index] = S;
S = 1.0f / S;
// calculate kalman gain K = PHS
@@ -100,7 +100,7 @@ void Ekf::fuseVelPosHeight()
_state.ang_error.setZero();
// fuse the observation
fuse(Kfusion, innovations[obs_index]);
fuse(Kfusion, _vel_pos_innov[obs_index]);
// correct the nominal quaternion
Quaternion dq;