Path: Orbit/OrbitMechanics
% Retrieve fuel budget information from a CAD model. Obtain data from thruster and fuel tank components as identified by fields within deviceInfo. -------------------------------------------------------------------------- Form: x = GetFuelBudgetDataFromCAD( g ) -------------------------------------------------------------------------- ------ Inputs ------ g (.) CAD data structure .deviceInfo.uECoefficient (1,2) Identifies a thruster .deviceInfo.massPressurant (1,2) Identifies a tank ------- Outputs ------- x .inr (3,3) Inertia matrix .cM (3,1) Center of mass .dryMass (1,1) Vehicle dry mass .thrusterData (.) Thruster data .r (3,:) Thruster position vectors .u (3,:) Thruster unit vectors .iSP (1,:) Specific impulse coeffs .thrust (1,:) Thrust coeffs .systemTemp (1,1) Tank temp .systemVol (1,1) Tank volume .systemMass (1,1) Fuel mass -------------------------------------------------------------------------- See also: DeviceProperties --------------------------------------------------------------------------
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