StdAtm:

Path: Common/Atmosphere

% Computes atmospheric density based on the standard atmosphere model.
 To get a table of standard atmosphere data type

 load -ascii AtmData;

 Type StdAtm for demo.
--------------------------------------------------------------------------
   Form:
   d = StdAtm( altitude, AtmData, units  )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   altitude   (:)     Altitude (m or ft)
   AtmData    (:,6)   Standard atmosphere data.
   units      (1,:)   'si', 'mks' or 'eng' i.e. m & kg or lb & ft

   -------
   Outputs
   -------
   d          (.)     Standard atmosphere struct
                      .temperature
                      .pressure
                      .density
                      .speedOfSound
                      .kinematicViscosity

--------------------------------------------------------------------------
 x is [altitude (m)  temperature (deg-K) pressure (N/m^2) density (kg/m^3)
       speed of sound (m/s) kinematic viscosity (m^2/s)]
 or
      [altitude (ft)  temperature (deg-R) pressure (lbf/ft^2) 
       density (lbf/m^3) speed of sound (ft/s) 
       kinematic viscosity (ft^2/s)]
--------------------------------------------------------------------------

Children:

AerospaceUtils: AeroData/AtmData
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle

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