diff --git a/src/shared/utils/AeroUtils/AeroUtils.cpp b/src/shared/utils/AeroUtils/AeroUtils.cpp
index a937551372be3dbd79ac7cfa9e849c04335be597..bd9f699214efad55a8ea2b20d5c95dd39847287d 100644
--- a/src/shared/utils/AeroUtils/AeroUtils.cpp
+++ b/src/shared/utils/AeroUtils/AeroUtils.cpp
@@ -71,15 +71,15 @@ float verticalSpeed(float p, float dpDt, float pRef, float tRef)
     return -(tRef * dpDt * powf(p / pRef, nInv)) / (a * n * p);
 }
 
-Vector2f geodetic2NED(const Vector2f& gpsData, const Vector2f& offset)
+Vector2f geodetic2NED(const Vector2f& target, const Vector2f& origin)
 {
     float mPerDegLat = 111132.95225;
     float mPerDegLon =
-        fabsf(111412.87733 * cosf(gpsData[0] * Constants::DEGREES_TO_RADIANS));
+        fabsf(111412.87733 * cosf(target[0] * Constants::DEGREES_TO_RADIANS));
 
     return {
-        mPerDegLat * (gpsData[0] - offset[0]),
-        mPerDegLon * (gpsData[1] - offset[1]),
+        mPerDegLat * (target[0] - origin[0]),
+        mPerDegLon * (target[1] - origin[1]),
     };
 }
 
diff --git a/src/shared/utils/AeroUtils/AeroUtils.h b/src/shared/utils/AeroUtils/AeroUtils.h
index ae170e3de0785fac4cb1734360e12531762cb983..e3e61661d46e90ee85f0de8b0a6b269683f316ba 100644
--- a/src/shared/utils/AeroUtils/AeroUtils.h
+++ b/src/shared/utils/AeroUtils/AeroUtils.h
@@ -173,12 +173,13 @@ float verticalSpeed(float p, float dpDt, float pRef, float tRef);
  * @brief Converts decimal degrees of latitude and longitude into displacement
  * in meters between two positions the with an ellipsoidal earth model.
  *
- * @param position1 Latitude and longitude of current position [lat lon][deg]
- * @param position2 Initial position used as an offset [lat lon][deg]
- * @return Distance between the two coordinates [n e][m]
+ * @param target Coordinates of target position [lat lon][deg]
+ * @param origin Coordinates of the Initial position used as the origin of the
+ * NED frame [lat lon][deg]
+ * @return Target NED position with respect to the origin coordinates [n e][m]
  */
-Eigen::Vector2f geodetic2NED(const Eigen::Vector2f& position1,
-                             const Eigen::Vector2f& position2);
+Eigen::Vector2f geodetic2NED(const Eigen::Vector2f& target,
+                             const Eigen::Vector2f& origin);
 
 /**
  * @brief Computes the rho (air density) of air at the given altitude.