diff options
Diffstat (limited to 'src/lib/external_lgpl/tecs/tecs.h')
-rw-r--r-- | src/lib/external_lgpl/tecs/tecs.h | 6 |
1 files changed, 3 insertions, 3 deletions
diff --git a/src/lib/external_lgpl/tecs/tecs.h b/src/lib/external_lgpl/tecs/tecs.h index 4fc009da9..d1ebacda1 100644 --- a/src/lib/external_lgpl/tecs/tecs.h +++ b/src/lib/external_lgpl/tecs/tecs.h @@ -71,10 +71,10 @@ public: // Update of the estimated height and height rate internal state // Update of the inertial speed rate internal state // Should be called at 50Hz or greater - void update_50hz(float baro_altitude, float airspeed, const math::Dcm &rotMat, const math::Vector3 &accel_body, const math::Vector3 &accel_earth); + void update_50hz(float baro_altitude, float airspeed, const math::Matrix<3,3> &rotMat, const math::Vector<3> &accel_body, const math::Vector<3> &accel_earth); // Update the control loop calculations - void update_pitch_throttle(const math::Dcm &rotMat, float pitch, float baro_altitude, float hgt_dem, float EAS_dem, float indicated_airspeed, float EAS2TAS, bool climbOutDem, float ptchMinCO, + void update_pitch_throttle(const math::Matrix<3,3> &rotMat, float pitch, float baro_altitude, float hgt_dem, float EAS_dem, float indicated_airspeed, float EAS2TAS, bool climbOutDem, float ptchMinCO, float throttle_min, float throttle_max, float throttle_cruise, float pitch_limit_min, float pitch_limit_max); // demanded throttle in percentage @@ -348,7 +348,7 @@ private: void _update_energies(void); // Update Demanded Throttle - void _update_throttle(float throttle_cruise, const math::Dcm &rotMat); + void _update_throttle(float throttle_cruise, const math::Matrix<3,3> &rotMat); // Detect Bad Descent void _detect_bad_descent(void); |