Most of the geostationary satellites already developed operate antenna pointing through fine orientation measurement and control of the satellite main body to which each antenna is rigidly attached. The main body orientation is measured by means of infrared Earth observation. Increasing antenna size and power and, sometimes, political constraints enhance the benefit of very accurate antenna pointing (0.05 deg, 3 a at antenna electrical axis level). This typically implies direct measurement of antenna orientation through the use of radio-frequency sensors incorporated in each antenna, mechanical decoupling between antennae to allow for compensation of structural deformations, and mechanical decoupling between each antenna and the satellite main body through the use of antenna pointing mechanisms to allow for high antenna control bandwidth. Concepts of antenna pointing mechanism and associated control for such satellites are presented shortly. Pointing performances of attitude control concepts alternatives are shown for a typical payload.
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