TrxCntrl:

Path: Orbit/OrbitManeuver

% Plans delta-v maneuvers to correct triaxial motion.
   Generates plots when called with no outputs.

--------------------------------------------------------------------------
   Form:
   [lonD0, lon0, dv, dvP, te, a] = TrxCntrl( eLon, lonTol )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   eLon                   East longitude of station (deg)
   lonTol                 Longitude tolerance (deg)

   -------
   Outputs
   -------
   lonD0                  Initial longitude rate at lon0
   lon0                   Starting longitude (will be ┬▒lonTol)
   dv                     Total delta-v requirement per year (m/sec)
   dvP                    Delta-v per maneuver (split into two) (m/sec)
   te                     Time between maneuvers (days)
   a                      Apparent acceleration (rad/day^2)

--------------------------------------------------------------------------
   References:	Michielsen, H.F., E.D. Webb, Stationkeeping of Stationary
               Satellites Made Simple, pp. 706-709.
--------------------------------------------------------------------------

Children:

Orbit: GravityModels/LoadGEM
Orbit: GravityModels/NormalizationMatrix
Orbit: GravityModels/UnnormalizeGravity
Orbit: OrbitManeuver/DVGeoTrx
Orbit: OrbitMechanics/AGravity
SC: SCMat/GEMT1
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/DispWithTitle
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/Mesh2
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Common: Graphics/TextS
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Math: Analysis/PDAL
Math: Analysis/SCHarm
Math: Linear/DupVect
Math: Linear/Factorl

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