Volume 37 Issue 8
Aug.  2018
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Du Dahua, He Erming, Wang Hui, Huang Hong. A New Modal Testing Technique for Light-weight Large Flexible Cable-net Structure[J]. Mechanical Science and Technology for Aerospace Engineering, 2018, 37(8): 1267-1271. doi: 10.13433/j.cnki.1003-8728.20180113
Citation: Du Dahua, He Erming, Wang Hui, Huang Hong. A New Modal Testing Technique for Light-weight Large Flexible Cable-net Structure[J]. Mechanical Science and Technology for Aerospace Engineering, 2018, 37(8): 1267-1271. doi: 10.13433/j.cnki.1003-8728.20180113

A New Modal Testing Technique for Light-weight Large Flexible Cable-net Structure

doi: 10.13433/j.cnki.1003-8728.20180113
  • Received Date: 2017-07-02
  • Publish Date: 2018-08-05
  • According to the structural features and dynamics characteristics of light-weight large flexible space cable-net antenna, a new modal testing technique is proposed in this study. A non-contact pneumatic excitation system is designed and applied to excite vibration, which is suitable for cable-net structure. The 3D scanning laser Doppler vibrometer (3D SLDV) is used to conduct non-contact vibration measurement. The structural modal parameters of cable-net antenna are identified based on the time domain modal analysis method of random decrement technique (RDT) combined with Ibrahim time domain method (ITD). As an extension to conventional modal test methods, the current technique has successfully obtained the vibration modes of a light-weight large flexible cable-net structure, showing a promising prospect of applications.
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