AirData:

Path: AerospaceUtils/AtmosphericCalculations

% Computes air data based on a simplified standard atmosphere model.
 If no arguments are specified it will plot m and q versus v and h.

 Type AirData for demo.
--------------------------------------------------------------------------
   Form:
   [m, q, rho, pS] = AirData( v, altitude, AtmData, units )
--------------------------------------------------------------------------

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

   -------
   Outputs
   -------
   m          (v,h)       Mach number
   q          (v,h)       Dynamic Pressure
   rho        h           Density
   pS         h           Static Pressure

--------------------------------------------------------------------------

Children:

AerospaceUtils: AeroData/AtmData
Common: Atmosphere/StdAtm
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS

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