Path: FormationFlying/DefaultData
% Generate a data structure for fuel tank info.
This is for a blow down system. Each tank has a set of thrusters
associated with the tank.
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Form:
tank = DefaultTankData( n )
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Inputs
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n (1,1) Number of tanks
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Outputs
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tank (.) Fuel tank data structure
.nThrusters (1,1) Number of thrusters
.minimumPulsewidth (1,1) Minimum width (s)
.pulsewidthResolution (1,1) Resolution (s)
.pressure (1,1) Pressure (N/m^2)
.thrustCoefficient (1,:) N/(N/m^2)
.massPressurant (1,1) Mass (kg)
.densityFuel (1,1) Density (kg/m^3)
.volumeTank (1,1) Volume (m^3)
.rPress (1,1) Gas constant
.temperatureTank (1,1) Temperature (deg-K)
.massFuel (1,1) Mass fuel (kg)
.uECoefficient (.) struct('iSP',{1,:},'pulsewidth',(1,:))
.r (3,:) Position from cm to thruster
.u (3,:) Force unit vector
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