I. Introduction
The promising perspective to provide high data rate communications links for a large variety of end users have become one of the main driver for new generation satellite communication systems at Ka band [1]. In mobile scenarios, where the antenna terminal is typically deployed on highly dynamic platforms such as airplanes, the system architecture needs to be low profile and lightweight to minimize its impact on the mechanical structure. Moreover, the antenna system in mobile scenarios has to track the satellite constantly in order to guarantee the service availability while moving. As a consequence of the indicated mechanical constraints, electrically steerable antennas are preferred over mechanical ones.