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Disturbance analysis and suppression of flexible antenna reflector on free-floating satellite antenna

  • School of Astronautics, Harbin Institute of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

To study the disturbance of flexible antenna reflector elastic deformation to free-floating satellite antenna, the fixed-interface component-mode synthesis method and Lagrange's equations are used. Under large motions, the rigid-flexible coupling dynamics model of satellite antenna is deduced through compatibility relations at the interface between axis end and antenna reflector. The model increases the computing efficiency without losing much accuracy. Then, satellite antenna dynamics is analyzed considering the antenna reflector as flexible body. Furthermore, the PD+ vibration force feedback control law is used to eliminate the system vibration, and the asymptotic stability of the system is proved based on Lyapunov method. The results show that the antenna excites the elastic vibration of flexible antenna reflector, which in turn causes its own jitter. This seriously affects the satellite antenna pointing accuracy. However, the proposed control strategy can quickly suppress system vibration. The above conclusion would have important academic value and engineering significance in the analysis and control of antenna pointing accuracy.

Original languageEnglish
Pages (from-to)2348-2356
Number of pages9
JournalHangkong Xuebao/Acta Aeronautica et Astronautica Sinica
Volume31
Issue number12
StatePublished - Dec 2010
Externally publishedYes

Keywords

  • Component-mode synthesis
  • Elastic vibration
  • Flexible antenna reflector
  • Satellite antenna
  • Vibration suppression

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