Oscillations caused by flexible attached elements of satellite constructions

Heading: 
Spacecraft Dynamics and Control
1Shatikhin, VE, 2Semenov, LP, 3Artemenko, YH, 4Borysenko, VM, 3Helenko, ОО
1Space Research Institute of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine, Kyiv, Ukraine
2State Space Agency of Ukraine, Kyiv, Ukraine
3Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
4State Space Agency of Ukraine, Kyiv, Ukraine; Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 2004, 10 ;(1):061-069
https://doi.org/10.15407/knit2004.01.061
Publication Language: Ukrainian
Abstract: 
We consider oscillations caused by flexible attached elements of satellite constructions, namely, solar array panels and antenna. An analysis of models of oscillations produced by solar array panels is carried out. We give some recommendations concerning the improvement of calculations of oscillations caused by flexible elements of satellite constructions with allowance made for modern achievements in the space materials science.
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