Abstract
This study presents the algorithm of a numerical analysis for pursuit-evasion type's differential games under the Stackelberg equilibrium. The Semi-DCNLP method is introduced as the optimizer for the solution of the flight path optimization under the Stackelberg equilibrium. For optimal flight path of the evader for an optimally pursuit spacecraft under the Stackelberg equilibrium, the Semi-DCNLP finds the proper trajectories which are corresponded with the trajectories obtained using the direct shooting method.
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