Yamal-200 spacecrafts attitude control by the signals of onboard repeater complex

On the basis of previously developed attitude control modes of Yamal-200 spacecrafts using inertial meters model, a mode was built that derives angular parameters from onboard repeater complex (ORC) signal processing. This paper proposes angular parameters generating circuit, structure and diagram of software & hardware package for the estimate of attitude control angles. This paper provides data on the implementation of this system in an actual product.