Economical unloading a gyro moment cluster of a land-survey mini-satellite attitude system at pulse-width control with delay

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For the land-survey mini-satellites we consider some problems on digital control of a gyro momemt cluster and its economical unloading from accumulated angular momentum by pulse-width control of magnetic driver and the plasma electro-reaction engines with physical delay.

Land-survey mini-satellite, pulse-width control, delay

Короткий адрес: https://sciup.org/148203496

IDR: 148203496

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