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fixed a typo
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@@ -87,7 +87,7 @@ float calc_true_airspeed_from_indicated(float speed_indicated, float pressure_am
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*
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* Note that the true airspeed is NOT the groundspeed, because of the effects of wind
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*
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* @param total_pressure pressure inside the pitot/prandl tube
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* @param total_pressure pressure inside the pitot/prandtl tube
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* @param static_pressure pressure at the side of the tube/airplane
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* @param temperature_celsius air temperature in degrees celcius
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* @return true airspeed in m/s
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@@ -78,7 +78,7 @@
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*
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* Note that the true airspeed is NOT the groundspeed, because of the effects of wind
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*
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* @param total_pressure pressure inside the pitot/prandl tube
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* @param total_pressure pressure inside the pitot/prandtl tube
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* @param static_pressure pressure at the side of the tube/airplane
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* @param temperature_celsius air temperature in degrees celcius
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* @return true airspeed in m/s
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