Added PerformanceModel for fixed wing (#22091)

* created a Performance Model for fixed wing vehicle
- added compensation for maximum climbrate, minimum sinkrate, minimum airspeed and trim airspeed based on weight ratio and air density
- added atmosphere lib to standard atmosphere calculations


---------

Signed-off-by: RomanBapst <bapstroman@gmail.com>
Co-authored-by: Thomas Stastny <thomas.stastny@auterion.com>

src/modules/ekf2/EKF/estimator_interface.h

@@ -71,7 +71,7 @@
 # include "sensor_range_finder.hpp"
 #endif // CONFIG_EKF2_RANGE_FINDER
 
-#include <lib/geo/geo.h>
+#include <lib/atmosphere/atmosphere.h>
 #include <matrix/math.hpp>
 #include <mathlib/mathlib.h>
 #include <mathlib/math/filter/AlphaFilter.hpp>
@@ -374,7 +374,7 @@ protected:
 	float _flow_max_distance{10.f};	///< maximum distance that the optical flow sensor can operate at (m)
 #endif // CONFIG_EKF2_OPTICAL_FLOW
 
-	float _air_density{CONSTANTS_AIR_DENSITY_SEA_LEVEL_15C};		// air density (kg/m**3)
+	float _air_density{atmosphere::kAirDensitySeaLevelStandardAtmos};		// air density (kg/m**3)
 
 	bool _imu_updated{false};      // true if the ekf should update (completed downsampling process)
 	bool _initialised{false};      // true if the ekf interface instance (data buffering) is initialized