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KIAM Preprint  59, Moscow, 2015
Authors: Belokonov I.V., Ivanov D. S., Ovchinnikov M. Y., Pen'kov V.I.
SamSat-QB50 Attitude Damping System
Abstract:
Nanosatellite attitude motion equipped with hysteretic dampers is studied. A number and size of the hysteretic rods is chose 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
Publication language: russian,  : 28
Research direction:
Theoretical and applied problems of mechanics
Russian source text:
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