TakeoffTransition:

Path: ACPro/ACPerformance

% Compute the radius and length of transition.
   The aircraft must reach the flight path angle at the screen height.
   hSc, n and gamma may be vectors but they must be the same length or
   of length 1.

   Type TakeoffTransition for a demo.
--------------------------------------------------------------------------
   Form:
   [s, v, r] = TakeoffTransition( hSc, n, gamma )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   hSc             (1,:) Screen height (m)
   n               (1,:) Lift/weight
   gamma           (1,:) Flight path angle (rad)

   -------
   Outputs
   -------
   s               (1,:) Length of transition (m)
   v               (1,:) Velocity (m/s)
   r               (1,:) Turning radius (m)

--------------------------------------------------------------------------
   Reference: Mair, W. and D. L. Birdsall, "Aircraft Performance,"
              Cambridge, p. 141-142.
--------------------------------------------------------------------------

Children:

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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