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@ -62,7 +62,7 @@ float calc_indicated_airspeed(float differential_pressure)
@@ -62,7 +62,7 @@ float calc_indicated_airspeed(float differential_pressure)
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if (differential_pressure > 0) { |
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return sqrtf((2.0f*differential_pressure) / CONSTANTS_AIR_DENSITY_SEA_LEVEL_15C); |
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} else { |
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return -sqrtf((2.0f*fabs(differential_pressure)) / CONSTANTS_AIR_DENSITY_SEA_LEVEL_15C); |
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return -sqrtf((2.0f*fabsf(differential_pressure)) / CONSTANTS_AIR_DENSITY_SEA_LEVEL_15C); |
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} |
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} |
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@ -106,6 +106,6 @@ float calc_true_airspeed(float total_pressure, float static_pressure, float temp
@@ -106,6 +106,6 @@ float calc_true_airspeed(float total_pressure, float static_pressure, float temp
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return sqrtf((2.0f*(pressure_difference)) / density); |
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} else |
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{ |
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return -sqrtf((2.0f*fabs(pressure_difference)) / density); |
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return -sqrtf((2.0f*fabsf(pressure_difference)) / density); |
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} |
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} |
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