Disturbance impulse effects on large umbrella space reflector dynamics

Manylion Llyfryddiaeth
Parent link:AIP Conference Proceedings
Vol. 1772 : Prospects of Fundamental Sciences Development (PFSD-2016).— 2016.— [060001, 7 p.]
Awdur Corfforaethol: Национальный исследовательский Томский политехнический университет (ТПУ) Институт физики высоких технологий (ИФВТ) Кафедра теоретической и прикладной механики (ТПМ)
Awduron Eraill: Belov S. Sergey, Zhukov A. Andrey, Pavlov M. S. Mikhail Sergeevich, Ponomarev S. Sergey
Crynodeb: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
Iaith:Saesneg
Cyhoeddwyd: 2016
Cyfres:Simulation and modeling in materials engineering
Pynciau:
Mynediad Ar-lein:http://dx.doi.org/10.1063/1.4964581
http://earchive.tpu.ru/handle/11683/35009
Fformat: Electronig Pennod Llyfr
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=652138

MARC

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200 1 |a Disturbance impulse effects on large umbrella space reflector dynamics  |f S. Belov [et al.] 
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300 |a Title screen 
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330 |a 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. 
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463 0 |0 (RuTPU)RU\TPU\network\17119  |t Vol. 1772 : Prospects of Fundamental Sciences Development (PFSD-2016)  |o XIII International Conference of Students and Young Scientists, 26–29 April 2016, Tomsk, Russia  |o [proceedings]  |f National Research Tomsk Polytechnic University (TPU) ; eds. A. Yu. Godymchuk (Godimchuk) ; L. Rieznichenko  |v [060001, 7 p.]  |d 2016 
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