mirror of https://github.com/ArduPilot/ardupilot
AP_TECS: Assume flight at cruise speed if speed measurement not available
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@ -391,12 +391,12 @@ void AP_TECS::_update_speed(float load_factor)
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// small time constant
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// small time constant
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}
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}
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// Get airspeed or default to halfway between min and max if
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// Get measured airspeed or default to trim speed and constrain to range between min and max if
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// airspeed is not being used and set speed rate to zero
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// airspeed sensor data cannot be used
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bool use_airspeed = _use_synthetic_airspeed_once || _use_synthetic_airspeed.get() || _ahrs.airspeed_sensor_enabled();
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bool use_airspeed = _use_synthetic_airspeed_once || _use_synthetic_airspeed.get() || _ahrs.airspeed_sensor_enabled();
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if (!use_airspeed || !_ahrs.airspeed_estimate(_EAS)) {
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if (!use_airspeed || !_ahrs.airspeed_estimate(_EAS)) {
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// If no airspeed available use average of min and max
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// If no airspeed available use average of min and max
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_EAS = 0.5f * (aparm.airspeed_min.get() + (float)aparm.airspeed_max.get());
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_EAS = constrain_float(0.01f * (float)aparm.airspeed_cruise_cm.get(), (float)aparm.airspeed_min.get(), (float)aparm.airspeed_max.get());
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}
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}
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// Implement a second order complementary filter to obtain a
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// Implement a second order complementary filter to obtain a
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