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Path: Orbit/OrbitMechanics
% Compute the power balance in a spacecraft.
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Form:
x = GetFuelBudgetDataFromCAD( g )
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Inputs
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g (1,1) CAD data structure
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Outputs
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x
.inr (3,3) Inertia matrix
.cM (3,1) Center of mass
.r (3,:) Thruster position vectors
.u (3,:) Thruster unit vectors
.f (1,:) Thruster data structure
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