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 r (3,:) Position vector (for eclipse calculations) 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: Graphics/AddFillToPlots Common: Graphics/Plot2D Common: Graphics/TimeLabl Common: Quaternion/QForm Common: Time/Date2JD
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