Path: ACPro/ACDesign
% Create a mass statement for an aircraft.
You pass in the mass of fuel and the datastructure with the aircraft
parameters.
Type AircraftGroupMassStatement for a demo.
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Form:
[m, g] = AircraftGroupMassStatement( mFuel, p, fileName )
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Inputs
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group (1,:) Group name
p (1,1) Data structure for the aircraft (optional)
fileName (1,:) File name for latex table
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Outputs
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m (1,:) Group mass (kg)
g {:} Group names
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See also AircraftGroupMass
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AC: Aircraft/AircraftGroupDataStructure AC: Aircraft/AircraftGroupMass Common: General/CreateLatexTable
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