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.
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Form:
x = GetFuelBudgetDataFromCAD( g )
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Inputs
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g (.) CAD data structure
.deviceInfo.uECoefficient (1,2) Identifies a thruster
.deviceInfo.massPressurant (1,2) Identifies a tank
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Outputs
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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
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See also: DeviceProperties
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