Pulse-width control of electro-reaction engines at correction of a satellite orbital motion

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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.

Correction of a satellite orbital motion, electro-reaction engine

Короткий адрес: https://sciup.org/148204326

IDR: 148204326

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