Path: Orbit/RHSOrbit

% Solar sail simulation right hand side.
   vargout = FSolarSail( t, x, flag, d )

   t                      Time
   x             (6,1)    The state vector [r;v]
   flag          (1,:)    Flags for ode113
   d             (1,1)    Data structure
                          .jDStart   (1,1) Julian date of simulation start
                          .muSun     (1,1) Central body gravitational parameter
                          .sail      (1,1) Sail data structure
                                           .normal (3,1) Sail normal
                                           .area   (1,1) Sail area
                                           .sigmaT (1,1) Sail transparency
                                           .sigmaA (1,1) Sail absorptivity
                                           .sigmaD (1,1) Sail diffusivity
                                           .sigmaS (1,1) Sail specular reflection
                          .mass      (1,1) Spacecraft mass
                          .planetsOn (1,1) 1 if planets are on

   xDot          (6,1)     The state vector derivative d[r;v]/dt



Orbit: OrbitMechanics/APlanet
SC: BasicOrbit/E2Nu
SC: BasicOrbit/M2E
SC: BasicOrbit/M2EApp
SC: BasicOrbit/M2EEl
SC: BasicOrbit/M2EHy
SC: BasicOrbit/M2Nu
SC: BasicOrbit/M2NuPb
SC: Ephem/PlanetPosition
SC: Ephem/Planets
SC: Ephem/SolarSys
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/TextS
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Time/DTSToDTA
Common: Time/Date2JD
Common: Time/JD2T
Math: Linear/DupVect
Math: Linear/Mag
Math: Linear/Unit

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