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PDE Modeling and Basic Vibration Control for Flexible Satellite

  • Zhijie Liu*
  • , Jinkun Liu
  • *Corresponding author for this work
  • University of Science and Technology Beijing

Research output: Chapter in Book/Report/Conference proceedingChapterpeer-review

Abstract

Satellites have gained much attention in the past decades for the purpose of remote sensing, communication and so on [8–10]. Considering a complex environment and space mission constraints, flexible satellite characterized by light weight structure, limitation of mass, low energy consumption and reduced launch cost, are widely used. Flexible satellites usually consists of a central rigid hub and long flexible appendages such as solar panels.

Original languageEnglish
Title of host publicationSpringer Tracts in Mechanical Engineering
PublisherSpringer
Pages25-43
Number of pages19
DOIs
StatePublished - 2020

Publication series

NameSpringer Tracts in Mechanical Engineering
ISSN (Print)2195-9862
ISSN (Electronic)2195-9870

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

  1. SDG 7 - Affordable and Clean Energy
    SDG 7 Affordable and Clean Energy

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