Commenting and formating fixes

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
This commit is contained in:
Silvan Fuhrer
2020-10-05 11:55:35 +02:00
parent 8f858d95e6
commit 5a184d2f5c
2 changed files with 9 additions and 10 deletions

View File

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