Исследование различных методов для решения задач оптимизации импульсных межпланетных перелетов «Земля — Марс»

Рассмотрены вопросы многоимпульсного орбитального перехода с оптимизацией расхода топлива в рамках задачи межпланетного перелета «Земля — Марс». Проанализированы и использованы различные методы для разработки многоимпульсных перелетов. Предложен метод проектирования многоимпульсных орбит с использованием прямого метода оптимизации с учетом итерационной стратегии. Предложен альтернативный способ, учитывающий связь между орбитами малой тяги и импульсными орбитами. В данной работе решается задача нелинейного программирования с использованием топливно-оптимальной траектории перелета с малой тягой для получения многоимпульсного локально оптимального решения. Получены результаты сходимости для задач нелинейного программирования.

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