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Diffstat (limited to 'src/modules/att_pos_estimator_ekf/KalmanNav.cpp')
-rw-r--r--src/modules/att_pos_estimator_ekf/KalmanNav.cpp20
1 files changed, 14 insertions, 6 deletions
diff --git a/src/modules/att_pos_estimator_ekf/KalmanNav.cpp b/src/modules/att_pos_estimator_ekf/KalmanNav.cpp
index 4ab41c6ce..9d3ef07f2 100644
--- a/src/modules/att_pos_estimator_ekf/KalmanNav.cpp
+++ b/src/modules/att_pos_estimator_ekf/KalmanNav.cpp
@@ -97,6 +97,14 @@ KalmanNav::KalmanNav(SuperBlock *parent, const char *name) :
{
using namespace math;
+ F.zero();
+ G.zero();
+ V.zero();
+ HAtt.zero();
+ RAtt.zero();
+ HPos.zero();
+ RPos.zero();
+
// initial state covariance matrix
P0.identity();
P0 *= 0.01f;
@@ -214,8 +222,8 @@ void KalmanNav::update()
if (correctAtt() == ret_ok) _attitudeInitCounter++;
if (_attitudeInitCounter > 100) {
- warnx("initialized EKF attitude\n");
- warnx("phi: %8.4f, theta: %8.4f, psi: %8.4f\n",
+ warnx("initialized EKF attitude");
+ warnx("phi: %8.4f, theta: %8.4f, psi: %8.4f",
double(phi), double(theta), double(psi));
_attitudeInitialized = true;
}
@@ -245,8 +253,8 @@ void KalmanNav::update()
// lat/lon and not have init
map_projection_init(lat0, lon0);
_positionInitialized = true;
- warnx("initialized EKF state with GPS\n");
- warnx("vN: %8.4f, vE: %8.4f, vD: %8.4f, lat: %8.4f, lon: %8.4f, alt: %8.4f\n",
+ warnx("initialized EKF state with GPS");
+ warnx("vN: %8.4f, vE: %8.4f, vD: %8.4f, lat: %8.4f, lon: %8.4f, alt: %8.4f",
double(vN), double(vE), double(vD),
lat, lon, double(alt));
}
@@ -625,7 +633,7 @@ int KalmanNav::correctAtt()
if (isnan(val) || isinf(val)) {
// abort correction and return
- warnx("numerical failure in att correction\n");
+ warnx("numerical failure in att correction");
// reset P matrix to P0
P = P0;
return ret_error;
@@ -691,7 +699,7 @@ int KalmanNav::correctPos()
if (!isfinite(val)) {
// abort correction and return
- warnx("numerical failure in gps correction\n");
+ warnx("numerical failure in gps correction");
// fallback to GPS
vN = _gps.vel_n_m_s;
vE = _gps.vel_e_m_s;