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KIAM Preprint № 26, Moscow, 2015
Authors: Ovchinnikov M. Y., Hao-Chi Chang, Mirer S. A., Roldugin D. S., Tkachev S. S.
Dynamical model of a satellite with controllable solar array
Satellite with 3DOF solar panel is considered. Satellite is a rigid bodies while solar panel consists of three parts connected by 1 DOF hinges. The work is aimed at the satellite-panel system attitude dynamical model construction.
complex structure, solar panel, 3DOF hinge, equations of motion
Publication language: english,  страниц: 19
Research direction:
Theoretical and applied problems of mechanics
English source text:
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