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[AeroUtils] Updated AeroUtils library with other functions

Emilio Corigliano requested to merge aeroutils-upd into main

Implemented functions in the AeroUtils library:

  • computeRho for calculating the air density at a given altitude;
  • computeSoundSpeed for calculating the speed of sound at a given altitude;
  • computeMach for calculating the mach given speed and altitude;

All heights are agl (above-ground-level) and the t0 is the temperature (in Kelvin) at height 0m agl. If we consider msl altitudes, the t0 to be passed is the MSL_TEMPERATURE that is 288.15 K.

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