New hybrid magnetic suspension vibration absorber with design, identification and control implementation

Chin E. Lin, C. C. Ker, R. T. Wang, C. L. Chen, B. C. Chen

Research output: Contribution to journalArticle

Abstract

This paper presents a new magnetic suspension vibration absorber. In the hybrid magnetic configuration, two permanent magnets are embedded into a stationary base and a motion support to result in a spring effect in the mechanical system, together with introducing an electromagnet to exert controllable force onto the motion support. To achieve the expected characteristics, system design for this magnetic suspension system is discussed. The equation of motion is described and modeled by considering magnetic spring effect, aluminum eddy current effect and air breath effect to apply feedback control to the system performance. System identification and modeling are discussed. The design is revised using magnetic field simulation before fabrication. Implementation and experiment are presented to demonstrate this vibration absorber system performance. This system is established for further control studies and application investigations.

Original languageEnglish
Pages (from-to)163-174
Number of pages12
JournalHangkong Taikong ji Minhang Xuekan/Journal of Aeronautics, Astronautics and Aviation
Volume39 A
Issue number3
Publication statusPublished - 2007 Sep 1

Fingerprint

magnetic suspension
Electromagnets
Eddy currents
Permanent magnets
Feedback control
Equations of motion
absorbers
vibration
Identification (control systems)
Systems analysis
Magnetic fields
Aluminum
Fabrication
Air
Experiments
electromagnets
system identification
eddy currents
feedback control
permanent magnets

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

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New hybrid magnetic suspension vibration absorber with design, identification and control implementation. / Lin, Chin E.; Ker, C. C.; Wang, R. T.; Chen, C. L.; Chen, B. C.

In: Hangkong Taikong ji Minhang Xuekan/Journal of Aeronautics, Astronautics and Aviation, Vol. 39 A, No. 3, 01.09.2007, p. 163-174.

Research output: Contribution to journalArticle

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