Path: FormationFlying/Collision
% Relative disturbances for use with a relative state. -------------------------------------------------------------------------- Form: aDiff = RelativeDisturb( jD, r, v, dr, dA, mSC, Cd, Cr, iRef ) -------------------------------------------------------------------------- ------ Inputs: ------- jD (1,1) Epoch (Julian date) r (3,1) Reference position in ECI frame (km) v (3,1) Reference velocity in ECI frame (km/s) dr (3,1) Relative position between the spacecraft (km) dA (1,1) Differential area between the spacecraft (m2) mSC (1,1) Mass spacecraft (kg) Cd (1,1) Drag coefficient Cr (1,1) Reflection coefficient iRef (1,1) Reference inclination (rad) ------- Outputs: -------- aDiff (3,1) sum of all the terms (m/s/s) --------------------------------------------------------------------------
AerospaceUtils: AtmosphericCalculations/AtmDens1 AerospaceUtils: AtmosphericCalculations/AtmDensTitan AerospaceUtils: AtmosphericCalculations/NeptuneDensity SC: Environs/MolWt2R SC: Ephem/SunV1 Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PlotDoubleYAxis Common: Graphics/PltStyle Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Time/DTSToDTA Common: Time/Date2JD Math: Linear/Mag Math: Linear/Unit Math: Trigonometry/CosD Math: Trigonometry/SinD
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