Path: Orbit/RHSOrbit
% Solar sail simulation right hand side.
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Form:
vargout = FSolarSail( t, x, flag, d )
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Inputs
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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
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Outputs
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xDot (6,1) The state vector derivative d[r;v]/dt
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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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