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Preprints of the Keldysh Institute of Applied Mathematics, 2015, 059, 28 pp. (Mi ipmp2021)  
SamSat-QB50 attitude damping system

I. V. Belokonov, D. S. Ivanov, M. Yu. Ovchinnikov, V. I. Pen'kov
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Abstract: Nanosatellite attitude motion equipped with hysteretic dampers is studied. A number and size of the hysteretic rods is choseт for achieving the aerodynamic orientation with defined accuracy. Laboratory investigation of hysteresis rods for nanosatellite is performed. The time of transit process in worst-case situation is estimated.
Keywords: hysteresis damper, stabilization.
Document Type: Preprint
Language: Russian
Citation: I. V. Belokonov, D. S. Ivanov, M. Yu. Ovchinnikov, V. I. Pen'kov, “SamSat-QB50 attitude damping system”, Keldysh Institute preprints, 2015, 059, 28 pp.
Citation in format AMSBIB
\Bibitem{BelIvaOvc15}
\by I.~V.~Belokonov, D.~S.~Ivanov, M.~Yu.~Ovchinnikov, V.~I.~Pen'kov
\paper SamSat-QB50 attitude damping system
\jour Keldysh Institute preprints
\yr 2015
\papernumber 059
\totalpages 28
\mathnet{http://mi.mathnet.ru/ipmp2021}
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    		Препринты Института прикладной математики им. М. В. Келдыша РАН
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