Path: Missions/LunarLanding
% Computes the fuel mass to achieve the desired acceleration vector. Type FuelMassFromAccel for a demo with a constant acceleration. -------------------------------------------------------------------------- Form: massFuel = FuelMassFromAccel( accel, dT, massDry, uE ) -------------------------------------------------------------------------- ------ Inputs ------ accel (1,:) Acceleration vector dT (1,:) Time vector massDry (1,1) Dry mass uE (1,1) Exhaust velocity ------- Outputs ------- massFuel (1,1) Fuel mass (kg) --------------------------------------------------------------------------
Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl
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