Path: ACPro/Trajectory
% Constant thrust and fuel consumption model
Returns constant thrust and specific fuel consumption.
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Form:
[thrust,fSp] = ThrustConstant( ~, ~, d )
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Inputs
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x (6,1) State vector (unused)
t (1,1) Time (unused)
d (.) Data structure
.thrust (1,1) Engine thrust (N)
.fSp (1,1) Specific fuel consumption (kg/Ns)
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Outputs
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thrust (1,1) Thrust (N)
fSp (1,1) Specific fuel consumption (kg/Ns)
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