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