Estimation of the mathematical model of the DC engine coupled with a reaction wheel

Abstract

Stabilization of the Microsatellite within the Centre of Space Technology is realized based on the control of the reaction wheels. In order to stabilize the microsatellites, it is necessary to choose the reaction wheels and also the mathematical modeling of the actuator system. In this paper, it was proposed to do the experimental identification of the mathematical model of the DC motor, coupled with the reaction wheel.