This paper solves the problem of the attitude control synthesis of elastic satellite with two solar panels. The equations of satellite motion around its center of gravity and bending vibrations. Experimental it proved that we can neglect the influence of the majority of natural vibration modes, except for the two forms of oscillations of solar panels in the plane xOy.
solar panels, attitude control synthesis, elastic satellite
"Metodyka syntezu upravlinnia oriientatsiieiu pruzhnoho suputnyka" [Methods of the attitude control synthesizing of the elastic satellite],
Systems of Arms and Military Equipment,