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| author | Anton Babushkin <anton.babushkin@me.com> | 2013-12-19 14:10:25 +0400 |
|---|---|---|
| committer | Anton Babushkin <anton.babushkin@me.com> | 2013-12-19 14:10:25 +0400 |
| commit | ba612c3ee8b88b9352e7cfa723997887dd736b76 (patch) | |
| tree | 8b101b50259ffebd4de12891f4f684d6d84c3f53 /src/lib/external_lgpl/tecs/tecs.cpp | |
| parent | e3a5a384d7b3678d1cbef63dc28fbe9a8f1de940 (diff) | |
| download | px4-firmware-ba612c3ee8b88b9352e7cfa723997887dd736b76.tar.gz px4-firmware-ba612c3ee8b88b9352e7cfa723997887dd736b76.tar.bz2 px4-firmware-ba612c3ee8b88b9352e7cfa723997887dd736b76.zip | |
mathlib fixes
Diffstat (limited to 'src/lib/external_lgpl/tecs/tecs.cpp')
| -rw-r--r-- | src/lib/external_lgpl/tecs/tecs.cpp | 6 |
1 files changed, 3 insertions, 3 deletions
diff --git a/src/lib/external_lgpl/tecs/tecs.cpp b/src/lib/external_lgpl/tecs/tecs.cpp index a733ef1d2..d7f350e5c 100644 --- a/src/lib/external_lgpl/tecs/tecs.cpp +++ b/src/lib/external_lgpl/tecs/tecs.cpp @@ -29,7 +29,7 @@ using namespace math; * */ -void TECS::update_50hz(float baro_altitude, float airspeed, const math::Dcm &rotMat, const math::Vector3 &accel_body, const math::Vector3 &accel_earth) +void TECS::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) { // Implement third order complementary filter for height and height rate // estimted height rate = _integ2_state @@ -257,7 +257,7 @@ void TECS::_update_energies(void) _SKEdot = _integ5_state * _vel_dot; } -void TECS::_update_throttle(float throttle_cruise, const math::Dcm &rotMat) +void TECS::_update_throttle(float throttle_cruise, const math::Matrix<3,3> &rotMat) { // Calculate total energy values _STE_error = _SPE_dem - _SPE_est + _SKE_dem - _SKE_est; @@ -468,7 +468,7 @@ void TECS::_update_STE_rate_lim(void) _STEdot_min = - _minSinkRate * CONSTANTS_ONE_G; } -void TECS::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 TECS::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) { |