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 Cet article a éte moissonné depuis la source Math-Net.Ru

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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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     title = {Yamal-200 spacecrafts attitude control by the signals of onboard repeater complex},
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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/

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[4] Sevast'yanov N. N., “Postroenie rezhimov orientatsii bez datchikov uglovoy skorosti na SS ‘Yamal-200’ ”, Vestnik Tomskogo gosudarstvennogo universiteta. Matematika i mekhanika, 2013, no. 3(23), 104–110 (in Russian) | MR

[5] Sevast'yanov N. N., “Povyshenie tochnosti rezhima inertsial'nogo upravleniya ‘prognoz’ ”, Vestnik Tomskogo gosudarstvennogo universiteta. Matematika i mekhanika, 2013, no. 6(26), 88–95 (in Russian)