ManeuverEnvelope:

Path: Orbit/OrbitManeuver

% Compute the maneuver envelope for a spacecraft rotating around another.
--------------------------------------------------------------------------
   Form:
   [p, r] = ManeuverEnvelope( f, m )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   f            (:,1)     Available force
   m            (1,1)     Mass

   -------
   Outputs
   -------
   p            (1,:)     Period
   r            (1,:)     Corresponding radius

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

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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