Path: CubeSat/Power
% CubeSat power analysis from batch orbit data. Simple batch calculation of power. Uses the same ephemeris model as RHSCubeSat. The built-in demo simulates a 1U satellite for one orbit. ------------------------------------------------------------------------ Form: [power] = CubeSatPowerAnalysis( d, q, r, jD ) CubeSatPowerAnalysis % demo ------------------------------------------------------------------------ ------ Inputs ------ d (.) Data structure from RHSCubeSat or SolarCellPower q (4,:) Quaternion, ECI to body v (3,:) Velocity vector jD (1,:) Julian dates ------- Outputs ------- power (1,:) Power produced by the solar cells ------------------------------------------------------------------------
AerospaceUtils: Coord/QLVLH CubeSat: Power/SolarCellPower SC: BasicOrbit/RVFromKepler SC: Ephem/Eclipse SC: Ephem/SunV1 Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/AddFillToPlots 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: Quaternion/Mat2Q Common: Quaternion/QForm Common: Time/DTSToDTA Common: Time/Date2JD Math: Linear/Cross Math: Linear/Dot Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit Math: Trigonometry/CosD Math: Trigonometry/SinD
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