AP_NavEKF: fixed check for airspeed sensor available
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@ -1768,7 +1768,8 @@ bool NavEKF::getLLH(struct Location &loc) const
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void NavEKF::OnGroundCheck()
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void NavEKF::OnGroundCheck()
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{
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{
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uint8_t lowAirSpd = (!_ahrs->airspeed_estimate_true(&VtasMeas) || VtasMeas < 8.0f);
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const AP_Airspeed *airspeed = _ahrs->get_airspeed();
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uint8_t lowAirSpd = (!airspeed || !airspeed->use() || airspeed->get_airspeed() * airspeed->get_EAS2TAS() < 8.0f);
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uint8_t lowGndSpd = (uint8_t)((sq(velNED[0]) + sq(velNED[1]) + sq(velNED[2])) < 4.0f);
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uint8_t lowGndSpd = (uint8_t)((sq(velNED[0]) + sq(velNED[1]) + sq(velNED[2])) < 4.0f);
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uint8_t lowHgt = (uint8_t)(fabsf(hgtMea < 15.0f));
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uint8_t lowHgt = (uint8_t)(fabsf(hgtMea < 15.0f));
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// Go with a majority vote from three criteria
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// Go with a majority vote from three criteria
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@ -1893,8 +1894,9 @@ void NavEKF::readAirSpdData()
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{
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{
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const AP_Airspeed *aspeed = _ahrs->get_airspeed();
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const AP_Airspeed *aspeed = _ahrs->get_airspeed();
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if (aspeed &&
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if (aspeed &&
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aspeed->last_update_ms() != lastAirspeedUpdate &&
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aspeed->use() &&
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_ahrs->airspeed_estimate_true(&VtasMeas)) {
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aspeed->last_update_ms() != lastAirspeedUpdate) {
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VtasMeas = aspeed->get_airspeed() * aspeed->get_EAS2TAS();
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lastAirspeedUpdate = aspeed->last_update_ms();
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lastAirspeedUpdate = aspeed->last_update_ms();
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newDataTas = true;
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newDataTas = true;
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RecallStates(statesAtVtasMeasTime, (IMUmsec - msecTasDelay));
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RecallStates(statesAtVtasMeasTime, (IMUmsec - msecTasDelay));
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