Disturbance impulse effects on large umbrella space reflector dynamics

Disturbance impulse effects on large umbrella space reflector dynamics

Bibliographic Details
Parent link:AIP Conference Proceedings
Vol. 1772 : Prospects of Fundamental Sciences Development (PFSD-2016).— 2016.— [060001, 7 p.]
Corporate Author: Национальный исследовательский Томский политехнический университет (ТПУ) Институт физики высоких технологий (ИФВТ) Кафедра теоретической и прикладной механики (ТПМ)
Other Authors: Belov S. Sergey, Zhukov A. Andrey, Pavlov M. S. Mikhail Sergeevich, Ponomarev S. Sergey
Summary:Title screen
Large umbrella space antennas are essential for communication, monitoring and observation of Earth and space objects. Despite investigations devoted to space antenna dynamics, the disturbance impulse shape effect on the root mean square error of spacecraft antenna reflecting surface has not been studied. This paper overcomes this gap describing disturbance impulse impact on root mean square error of spacecraftantenna reflecting surface relative to paraboloid via nonlinear finite element method. Based on numerical results root mean square dependency on disturbance time for rectangular and sine impulses was calculated. This approach could be applied in studying antenna reflecting surface response on disturbance impulse for different types of perspective large space antennas.
Режим доступа: по договору с организацией-держателем ресурса
Published: 2016
Series:Simulation and modeling in materials engineering
Subjects:
электронный ресурс
труды учёных ТПУ
вибрации
импульсные воздействия
отражатели
космические антенны
космические объекты
космические корабли
отражающие поверхности
метод конечных элементов
Online Access:http://dx.doi.org/10.1063/1.4964581
http://earchive.tpu.ru/handle/11683/35009
Format: Electronic Book Chapter
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=652138

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