DVIDrift:

Path: Orbit/OrbitManeuver

% Computes inclination drift for geosynchronous orbits.
   Use this function to plan north/south stationkeeping.
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   Form:
   [dV, dT, dI] = DVIDrift( box, year, doPlot )
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   ------
   Inputs
   ------
   box    (1,1) Size of stationkeeping box (deg)
   year   (1,:) Year of maneuvers
   doPlot (1,1) Create a plot


   -------
   Outputs
   -------
   dV    (1,1) Delta V per maneuver (m/sec)
   dT    (1,:) Time between maneuvers (days)
   dI    (1,:) Change in inclination

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   Reference:   Agrawal, B. N. (1986). Design of Geosynchronous Spacecraft. 
                Prentice-Hall, Englewood Cliffs, NJ.
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Children:

Common: Graphics/Plot2D

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