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-baПоказать полностьюsed 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.

Журнал: Journal of Physics: Conference Series

Выпуск журнала: 1050

Номера страниц: 012042

Издатель: Institute of Physics Publishing

• 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)

• Ядро РИНЦ (eLIBRARY.RU)