Nonlinear Oscillations of Elastic Solar Panels of a Spacecraft at Finite Turn by Roll
- Авторы: Russkikh S.V.1, Shklyurchuk F.N.2
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Учреждения:
- Moscow Aviation Institute (National Research University)
- Institute of Applied Mechanics of the Russian Academy of Sciences
- Выпуск: Том 53, № 2 (2018)
- Страницы: 147-155
- Раздел: Article
- URL: https://ogarev-online.ru/0025-6544/article/view/163242
- DOI: https://doi.org/10.3103/S0025654418020048
- ID: 163242
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Аннотация
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.
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Об авторах
S. Russkikh
Moscow Aviation Institute (National Research University)
Автор, ответственный за переписку.
Email: sergey.russkih@rambler.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
F. Shklyurchuk
Institute of Applied Mechanics of the Russian Academy of Sciences
Email: sergey.russkih@rambler.ru
Россия, Leningradskii pr. 7, Moscow, 125040
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