Abstract
РЕШЕНИЕ ЗАДАЧИ ОПТИМАЛЬНОЙ КОРРЕКЦИИ УГЛОВЫХ ЭЛЕМЕНТОВ ОРБИТЫ КОСМИЧЕСКОГО АППАРАТА С ИСПОЛЬЗОВАНИЕМ КВАТЕРНИОННОГО УРАВНЕНИЯ ОРИЕНТАЦИИ ОРБИТЫ
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Schedule a callMore From: Izvestiya of Saratov University. New Series. Series: Mathematics. Mechanics. Informatics
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