more fixes for the airspeed readout

1 files changed, 34 insertions, 35 deletions

diff --git a/apps/systemlib/airspeed.h b/apps/systemlib/airspeed.h
index b1beb79ae..088498943 100644
--- a/apps/systemlib/airspeed.h
+++ b/apps/systemlib/airspeed.h
@@ -48,43 +48,42 @@
 
  __BEGIN_DECLS
  
-/**
- * Calculate indicated airspeed.
- *
- * 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
- * the true airspeed.
- *
- * @param pressure_front pressure inside the pitot/prandl tube
- * @param pressure_ambient pressure at the side of the tube/airplane
- * @param temperature air temperature in degrees celcius
- * @return indicated airspeed in m/s
- */
-__EXPORT float calc_indicated_airspeed(float pressure_front, float pressure_ambient, float temperature);
+ /**
+  * Calculate indicated airspeed.
+  *
+  * 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
+  * the true airspeed.
+  *
+  * @param total_pressure pressure inside the pitot/prandtl tube
+  * @param static_pressure pressure at the side of the tube/airplane
+  * @return indicated airspeed in m/s
+  */
+ __EXPORT float calc_indicated_airspeed(float differential_pressure);
  
-/**
- * Calculate true airspeed from indicated airspeed.
- *
- * Note that the true airspeed is NOT the groundspeed, because of the effects of wind
- *
- * @param speed current indicated airspeed
- * @param pressure_ambient pressure at the side of the tube/airplane
- * @param temperature air temperature in degrees celcius
- * @return true airspeed in m/s
- */
-__EXPORT float calc_true_airspeed_from_indicated(float speed, float pressure_ambient, float temperature);
+ /**
+  * Calculate true airspeed from indicated airspeed.
+  *
+  * Note that the true airspeed is NOT the groundspeed, because of the effects of wind
+  *
+  * @param speed_indicated current indicated airspeed
+  * @param pressure_ambient pressure at the side of the tube/airplane
+  * @param temperature_celsius air temperature in degrees celcius
+  * @return true airspeed in m/s
+  */
+ __EXPORT float calc_true_airspeed_from_indicated(float speed_indicated, float pressure_ambient, float temperature_celsius);
  
-/**
- * Directly calculate true airspeed
- *
- * Note that the true airspeed is NOT the groundspeed, because of the effects of wind
- *
- * @param pressure_front pressure inside the pitot/prandl tube
- * @param pressure_ambient pressure at the side of the tube/airplane
- * @param temperature air temperature in degrees celcius
- * @return true airspeed in m/s
- */
-__EXPORT float calc_true_airspeed(float pressure_front, float pressure_ambient, float temperature);
+ /**
+  * Directly calculate true airspeed
+  *
+  * 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 static_pressure pressure at the side of the tube/airplane
+  * @param temperature_celsius air temperature in degrees celcius
+  * @return true airspeed in m/s
+  */
+ __EXPORT float calc_true_airspeed(float total_pressure, float static_pressure, float temperature_celsius);
 
 __END_DECLS