Abstract
Description of magnetic control system of the microsatellite “Micron” is represented. Microsatellite developed in State Design Office “Yuzhnoye” in accordance with plans of experimental-design works of National Space Agency of Ukraine. Control system developed in scientific manufacturing company “Hartron-CONSAT” Main attention in the paper is devoted to problems of high-performance algorithms designing on estimation parameters of the satellite by means of magneto meter measurements. The series of new results, obtained during the designing of control system, allowed to solve successfully the problems for estimation of satellite motion parameters by magnetometer information is represented. The efficiency of suggested algorithms is confmned by simulation results.
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