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AP_TECS: adapt for new airspeed variable names

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This commit is contained in:
Andrew Tridgell 2013-07-18 11:56:06 +10:00
parent 42d107b0d9
commit fb0e48a25d
1 changed files with 3 additions and 3 deletions
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6
libraries/AP_TECS/AP_TECS.cpp
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@ -196,8 +196,8 @@ void AP_TECS::_update_speed(void)
float EAS2TAS = _baro->get_EAS2TAS(); float EAS2TAS = _baro->get_EAS2TAS();
_TAS_dem = _EAS_dem * EAS2TAS; _TAS_dem = _EAS_dem * EAS2TAS;
_TASmax = aparm.flybywire_airspeed_max * EAS2TAS; _TASmax = aparm.airspeed_max * EAS2TAS;
_TASmin = aparm.flybywire_airspeed_min * EAS2TAS; _TASmin = aparm.airspeed_min * EAS2TAS;
// Reset states of time since last update is too large // Reset states of time since last update is too large
if (DT > 1.0) { if (DT > 1.0) {
@ -211,7 +211,7 @@ void AP_TECS::_update_speed(void)
// airspeed is not being used and set speed rate to zero // airspeed is not being used and set speed rate to zero
if (!_ahrs->airspeed_sensor_enabled() || !_ahrs->airspeed_estimate(&_EAS)) { if (!_ahrs->airspeed_sensor_enabled() || !_ahrs->airspeed_estimate(&_EAS)) {
// If no airspeed available use average of min and max // If no airspeed available use average of min and max
_EAS = 0.5f * (aparm.flybywire_airspeed_min + aparm.flybywire_airspeed_max); _EAS = 0.5f * (aparm.airspeed_min + aparm.airspeed_max);
} }
// Implement a second order complementary filter to obtain a // Implement a second order complementary filter to obtain a