mirror of https://github.com/ArduPilot/ardupilot
AP_TECS: protect against low airspeed in reset
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@ -383,9 +383,13 @@ void AP_TECS::_update_speed(float load_factor)
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_TASmin = _TAS_dem;
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}
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// limit the airspeed to a minimum of 3 m/s
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const float min_airspeed = 3.0;
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// Reset states of time since last update is too large
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if (DT > 1.0f) {
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_TAS_state = (_EAS * EAS2TAS);
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_TAS_state = MAX(_TAS_state, min_airspeed);
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_integDTAS_state = 0.0f;
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DT = 0.1f; // when first starting TECS, use a
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// small time constant
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@ -411,8 +415,7 @@ void AP_TECS::_update_speed(float load_factor)
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_integDTAS_state = _integDTAS_state + integDTAS_input * DT;
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float TAS_input = _integDTAS_state + _vel_dot + aspdErr * _spdCompFiltOmega * 1.4142f;
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_TAS_state = _TAS_state + TAS_input * DT;
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// limit the airspeed to a minimum of 3 m/s
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_TAS_state = MAX(_TAS_state, 3.0f);
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_TAS_state = MAX(_TAS_state, min_airspeed);
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}
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