Path: LunarMissions/LunarLanding
% Cost for the landing for a 3D planet problem.
The cost is the weighted sum of total time and fuel mass.
This is computed from the decision variable.
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Form:
cost = LandingCost3D( x, d )
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Inputs
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x (:,1) [beta;alpha;thrust;dT]
d (.) Data structure describing spacecraft model
.timeW (1,1) Time weight
.fuelW (1,1) Fuel weight
.uE (1,1) Exhaust velocity
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Outputs
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cost (1,1) Time weighted with total fuel consumed
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