Path: SpacecraftEstimation/DemoFuns
% Right-hand-side for an isothermal spacecraft model. This is a wrapper function for RHSIsothermal -------------------------------------------------------------------------- Form: f = RHSIsothermalUKF( x, t, u ) -------------------------------------------------------------------------- ------ Inputs ------ x (1,1) State [t] t (1,1) Time (not used) u (1,1) Data structure ------- Outputs ------- f (1,1) State derivative --------------------------------------------------------------------------
SC: BasicOrbit/Period SC: BasicOrbit/RVFromKepler SC: Environs/EarthAlb SC: Environs/EarthRad SC: Environs/SolarFlx SC: Ephem/Eclipse SC: Ephem/SunV1 Thermal: ThermalAnalysis/RHSIsothermal Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/IsVersionAfter Common: General/MatToCell Common: General/StringToTokens Common: General/Watermark Common: Graphics/NPlot Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/Plot3D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/FindSolsticeOrEquinox Math: Linear/Dot Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit Math: Trigonometry/CosD Math: Trigonometry/SinD
Back to the SpacecraftEstimation Module page