
We present a method for a station-keeping of a small land-survey satellite on a sun-synchronous orbit with respect to longitude of ascending node. We have developed algorithms for a pulse-width control of the correcting engine unit with 8 electro-reaction engines and have presented the research results for created algorithms.
Представляется метод удержания малого спутника землеобзора на солнечно-синхронной орбите по долготе восходящего узла. Созданы алгоритмы широтно-импульсного управления КДУ с 8 электрореактивными двигателями и приведены результаты исследования разработанных алгоритмов.
КОРРЕКЦИЯ ОРБИТАЛЬНОГО ДВИЖЕНИЯ СПУТНИКА,ЭЛЕКТРОРЕАКТИВНЫЙ ДВИГАТЕЛЬ,CORRECTION OF A SATELLITE ORBITAL MOTION,ELECTRO-REACTION ENGINE
КОРРЕКЦИЯ ОРБИТАЛЬНОГО ДВИЖЕНИЯ СПУТНИКА,ЭЛЕКТРОРЕАКТИВНЫЙ ДВИГАТЕЛЬ,CORRECTION OF A SATELLITE ORBITAL MOTION,ELECTRO-REACTION ENGINE
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