mirror of https://github.com/ArduPilot/ardupilot
AP_Baro: Avoid returning 0.0f for EAS2TAS
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@ -319,7 +319,11 @@ float AP_Baro::get_EAS2TAS(void)
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// provides a more consistent reading then trying to estimate a complete
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// ISA model atmosphere
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float tempK = get_ground_temperature() + C_TO_KELVIN - ISA_LAPSE_RATE * altitude;
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_EAS2TAS = safe_sqrt(SSL_AIR_DENSITY / ((float)get_pressure() / (ISA_GAS_CONSTANT * tempK)));
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const float eas2tas_squared = SSL_AIR_DENSITY / ((float)get_pressure() / (ISA_GAS_CONSTANT * tempK));
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if (!is_positive(eas2tas_squared)) {
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return 1.0;
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}
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_EAS2TAS = sqrtf(eas2tas_squared);
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_last_altitude_EAS2TAS = altitude;
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return _EAS2TAS;
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}
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