Geodesic
Yamal-200 spacecrafts attitude control by the signals of onboard repeater complex
Vestnik Tomskogo gosudarstvennogo universiteta. Matematika i mehanika, no. 1 (2014), pp. 117-124

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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.
Mots-clés : orientation mode, signal amplitude.
Keywords: analysis of changes in capacity, control reliability, signal spectrum analyzer 
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     author = {N. N. Sevast'yanov},
     title = {Yamal-200 spacecrafts attitude control by the signals of onboard repeater complex},
     journal = {Vestnik Tomskogo gosudarstvennogo universiteta. Matematika i mehanika},
     pages = {117--124},
     publisher = {mathdoc},
     number = {1},
     year = {2014},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/VTGU_2014_1_a11/}
}
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N. N. Sevast'yanov. Yamal-200 spacecrafts attitude control by the signals of onboard repeater complex. Vestnik Tomskogo gosudarstvennogo universiteta. Matematika i mehanika, no. 1 (2014), pp. 117-124. http://geodesic.mathdoc.fr/item/VTGU_2014_1_a11/