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Интеллектуальная Система Тематического Исследования НАукометрических данных |
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In this talk, we consider a problem on the rocket flight final height maximization under the control and endpoint constraints. The problem is considered on a constrained time interval, filling the gap between problems on free and fixed time interval. Using Pontryagin Maximum Principle, we obtain all types of optimal trajectories and then construct optimal synthesis. In addition, we investigate evolution of obtained synthesis w.r.t problem parameters.