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Commenting and formating fixes
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
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@@ -58,7 +58,7 @@ enum AIRSPEED_COMPENSATION_MODEL {
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};
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/**
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* Calculate indicated airspeed (IAS).
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* Calculate indicated airspeed (IAS) and correct for friction inside pitot and tube.
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*
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* Note that the indicated airspeed is not the true airspeed because it
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* lacks the air density compensation. Use the calc_true_airspeed functions to get
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@@ -88,7 +88,7 @@ __EXPORT float calc_IAS(float differential_pressure);
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/**
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* Calculate true airspeed (TAS) from calibrated airspeed (CAS).
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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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* Note that the true airspeed is NOT the groundspeed, because of the effects of wind.
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*
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* @param speed_equivalent current calibrated airspeed
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* @param pressure_ambient pressure at the side of the tube/airplane
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@@ -109,7 +109,7 @@ __EXPORT float calc_CAS_from_IAS(float speed_indicated, float scale);
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/**
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* Directly calculate true airspeed (TAS)
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* Directly calculate true airspeed (TAS).
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*
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* Here we assume to have no instrument or pitot position error (IAS = CAS).
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* Note that the true airspeed is NOT the groundspeed, because of the effects of wind.
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@@ -133,7 +133,6 @@ __EXPORT float get_air_density(float static_pressure, float temperature_celsius)
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* Calculate calibrated airspeed (CAS) from true airspeed (TAS).
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* It is the inverse function to calc_TAS_from_CAS()
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*
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*
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* @param speed_true current true airspeed
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* @param pressure_ambient pressure at the side of the tube/airplane
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* @param temperature_celsius air temperature in degrees celcius
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