A more accurate modeling of the effects of actuators in large space structures

The present paper deals with finite actuators. A nonspinning three-axis stabilized space vehicle having a two-dimensional large structure and a rigid body at the center is chosen for analysis. The torquers acting on the vehicle are modeled as antisymmetric forces distributed in a small but finite area. In the limit they represent point torquers which also are treated as a special case of surface distribution of dipoles. Ordinary and partial differential equations governing the forced vibrations of the vehicle are derived by using the Hamilton's principle. Associated modal inputs are obtained for both the distributed moments and the distributed forces. We show that the finite torquers excite the higher modes less than the point torquers. Modal Cost Analysis proves to be a suitable methodology to this end.