Path: SC/Actuator
% BatterySize Battery sizing for a given orbit and array power. Type BatterySize for a demo. -------------------------------------------------------------------------- Form: [m, v, b] = BatterySize( sma, inc, power, jD0, dOD, rhoM, rhoV ) -------------------------------------------------------------------------- ------ Inputs ------ sma (1,1) Semi-major axis (km) inc (1,1) Inclination (rad) power (1,1) Solar array power (W) jD0 (1,1) Start Julian day number (day) dOD (1,1) Depth of discharge (0 to 1) rhoM (1,1) Specific power (W-h/kg) rhoV (1,1) Energy density (W-h/L) ------- Outputs ------- m (1,1) Mass (kg) v (1,1) Volume (L) b (1,1) Battery capacity (W-h) --------------------------------------------------------------------------
Orbit: OrbitCoord/SLR Orbit: OrbitMechanics/RVOrbGen SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: Ephem/Eclipse SC: Ephem/SunV1 Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Mesh2 Common: Graphics/NPlot Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/DTSToDTA Common: Time/Date2JD Math: Linear/Dot Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit Math: Trigonometry/CosD Math: Trigonometry/SinD
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