US76 atmospheric density (convenience function)
[dens] = CL_mod_atmUS76Density(alt)
Computes the density at a given altitude using the US76 atmospheric model.
Notes:
- The model can be used for altitudes in [0, 1000] km.
- Results for altitudes outside this range are set to %nan.
Altitude [m] (1xN)
Density [kg/m^3] (1xN)
CNES - DCT/SB