Nonlinear dynamic modelling and performance of deployable telescopic tubular mast (TTM)

Tongtong Sun, Paolo Gasbarri, Lin Du, Zichen Deng

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The aim of this work is to present the longitude and transverse vibrations of a deployable TTM, which is attached on a spacecraft system, considering the effect of rigid-flexible coupling phenomenon. The proposed model is derived based on the principle of virtual work and discretized by assumed mode method. To introduce the nonlinear effect, the von Kármán strain is adopted. Additionally, locking and restart behaviors are taken into account in the modelling procedure of the deploying process. Finally, the dynamic phenomena of the longitude and transverse displacements are analyzed at different deploying velocities.

Original languageEnglish
Title of host publicationAerospace Science and Engineering – IV Aerospace PhD-Days
EditorsAndrea Alaimo, Antonio Esposito, Marco Petrolo
PublisherAssociation of American Publishers
Pages72-75
Number of pages4
ISBN (Print)9781644903186
DOIs
StatePublished - 2024
Event4th Aerospace PhD-Days 2024, International Congress of PhD Students in Aerospace Science and Engineering - Scopello, Italy
Duration: 6 May 20249 May 2024

Publication series

NameMaterials Research Proceedings
Volume42
ISSN (Print)2474-3941
ISSN (Electronic)2474-395X

Conference

Conference4th Aerospace PhD-Days 2024, International Congress of PhD Students in Aerospace Science and Engineering
Country/TerritoryItaly
CityScopello
Period6/05/249/05/24

Keywords

  • Deploying Process
  • Flexible Vibration
  • Nonlinear Dynamics
  • Telescopic Tubular Mast

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