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| author | Lorenz Meier <lm@inf.ethz.ch> | 2013-10-10 21:15:03 +0200 |
|---|---|---|
| committer | Lorenz Meier <lm@inf.ethz.ch> | 2013-10-10 21:15:03 +0200 |
| commit | 44deeb85c09451865c7d869f495a31f1b4348fec (patch) | |
| tree | 4022df1d50a5d9b2d5cbbc05c5e56289965fc25a /src/modules/att_pos_estimator_ekf/KalmanNav.hpp | |
| parent | 0cb8e782b0e2a6ca0dde4fac641e863c95d04511 (diff) | |
| download | px4-firmware-44deeb85c09451865c7d869f495a31f1b4348fec.tar.gz px4-firmware-44deeb85c09451865c7d869f495a31f1b4348fec.tar.bz2 px4-firmware-44deeb85c09451865c7d869f495a31f1b4348fec.zip | |
We compile with GCC 4.7.4
Diffstat (limited to 'src/modules/att_pos_estimator_ekf/KalmanNav.hpp')
| -rw-r--r-- | src/modules/att_pos_estimator_ekf/KalmanNav.hpp | 26 |
1 files changed, 13 insertions, 13 deletions
diff --git a/src/modules/att_pos_estimator_ekf/KalmanNav.hpp b/src/modules/att_pos_estimator_ekf/KalmanNav.hpp index f01ee0355..799fc2fb9 100644 --- a/src/modules/att_pos_estimator_ekf/KalmanNav.hpp +++ b/src/modules/att_pos_estimator_ekf/KalmanNav.hpp @@ -166,19 +166,19 @@ protected: double lat, lon; /**< lat, lon radians */ float alt; /**< altitude, meters */ // parameters - control::BlockParam<float> _vGyro; /**< gyro process noise */ - control::BlockParam<float> _vAccel; /**< accelerometer process noise */ - control::BlockParam<float> _rMag; /**< magnetometer measurement noise */ - control::BlockParam<float> _rGpsVel; /**< gps velocity measurement noise */ - control::BlockParam<float> _rGpsPos; /**< gps position measurement noise */ - control::BlockParam<float> _rGpsAlt; /**< gps altitude measurement noise */ - control::BlockParam<float> _rPressAlt; /**< press altitude measurement noise */ - control::BlockParam<float> _rAccel; /**< accelerometer measurement noise */ - control::BlockParam<float> _magDip; /**< magnetic inclination with level */ - control::BlockParam<float> _magDec; /**< magnetic declination, clockwise rotation */ - control::BlockParam<float> _g; /**< gravitational constant */ - control::BlockParam<float> _faultPos; /**< fault detection threshold for position */ - control::BlockParam<float> _faultAtt; /**< fault detection threshold for attitude */ + control::BlockParamFloat _vGyro; /**< gyro process noise */ + control::BlockParamFloat _vAccel; /**< accelerometer process noise */ + control::BlockParamFloat _rMag; /**< magnetometer measurement noise */ + control::BlockParamFloat _rGpsVel; /**< gps velocity measurement noise */ + control::BlockParamFloat _rGpsPos; /**< gps position measurement noise */ + control::BlockParamFloat _rGpsAlt; /**< gps altitude measurement noise */ + control::BlockParamFloat _rPressAlt; /**< press altitude measurement noise */ + control::BlockParamFloat _rAccel; /**< accelerometer measurement noise */ + control::BlockParamFloat _magDip; /**< magnetic inclination with level */ + control::BlockParamFloat _magDec; /**< magnetic declination, clockwise rotation */ + control::BlockParamFloat _g; /**< gravitational constant */ + control::BlockParamFloat _faultPos; /**< fault detection threshold for position */ + control::BlockParamFloat _faultAtt; /**< fault detection threshold for attitude */ // status bool _attitudeInitialized; bool _positionInitialized; |