A. B. Nuralieva, S. S. Tkachev, “Mathematical model for a satellite with flexible 1DOF hinged solar panel”, Keldysh Institute preprints, 2015,061, 19 pp.

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Mathematical model for a satellite with flexible 1DOF hinged solar panel

A. B. Nuralieva, S. S. Tkachev

Abstract: Mathematical model of a satellite with flexible 1DOF hinged solar panel is considered. Nonlinear and linearized equations are derived. Model verification using first integrals of motion and normal modes is carried out.

Keywords: flexible element, normal mode, model verification.