Path: Interplanetary/OrbitInsertion
% Cost for the landing for a 2D orbit problem. The cost is the total acceleration for the maneuver. This is computed from the decision variable. -------------------------------------------------------------------------- Form: cost = ApproachCost2D( u, ~ ) -------------------------------------------------------------------------- ------ Inputs ------ u (2,:) [phi;a] ------- Outputs ------- cost (1,1) Total acceleration --------------------------------------------------------------------------
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