Nonlinear Oscillations of Elastic Solar Panels of a Spacecraft at Finite Turn by Roll


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Resumo

Non-stationary rotational motion and nonlinear oscillations in the roll plane of a spacecraft with two elastic panels of solar batteries are considered. The spacecraft and sections of solar panels are considered to be non-deformable; they are interconnected by elastic-hinged joints that allow large angles of rotation. The spacecraft makes a turn about its axis as a solid body. Motion of elastic system under consideration is described in a connected coordinate system. Equations of motion are obtained on the basis of principle of possible displacements. Examples of numerical integration of a system of nonlinear differential equations with the analysis of convergence are given.

Sobre autores

S. Russkikh

Moscow Aviation Institute (National Research University)

Autor responsável pela correspondência
Email: sergey.russkih@rambler.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993

F. Shklyurchuk

Institute of Applied Mechanics of the Russian Academy of Sciences

Email: sergey.russkih@rambler.ru
Rússia, Leningradskii pr. 7, Moscow, 125040

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