Тип публикации: доклад, тезисы доклада, статья из сборника материалов конференций
Конференция: Mechanical Science and Technology Update 2018, MSTU 2018; Omsk; Omsk
Год издания: 2018
Идентификатор DOI: 10.1088/1742-6596/1050/1/012042
Аннотация: High reliability is required for the deployment of the transformable structures as this process is crucial for successful spacecraft mission. Computational evaluation of the reliability parameters for the deployment is of a great importance as it is not possible to fully reproduce the real conditions of outer space during ground-based tests. The presented approach to estimate the probability of failure-free deployment is based on the condition of exceeding the driving torque over the resisting moment at each of the angular positions of the structure. The approach was used to compute the reliability functions for deployment of a space reflector. The calculations were carried out based on kinematic and dynamic analysis of the structure.
Издание
Журнал: Journal of Physics: Conference Series
Выпуск журнала: 1050
Номера страниц: 012042
Издатель: Institute of Physics Publishing
Персоны
- Lepikhin A.M. (Institute of Computational Technologies, Siberian Branch of the Russian Academy of Sciences)
- Burov A.E. (Institute of Computational Technologies, Siberian Branch of the Russian Academy of Sciences)
- Pokhabov Y.P. (Institute of Computational Technologies, Siberian Branch of the Russian Academy of Sciences)
Вхождение в базы данных
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