Electromagnet Actuator Analysis of Magnetic Levitation System

자기부상시스템의 전자석 구동기 해석

  • Kim, Chan-Jo (Dept.of Aerospace Engineeing, Graduate School of Busan National University) ;
  • Cho, Kyeum-Rae (Dept.of Aerospace Engineeing, Graduate School of Busan National University)
  • 김찬조 (부산대학교 항공우주공학과 대학원) ;
  • 조겸래 (부산대학교 항공우주공학과, 기계기술연구소)
  • Published : 2000.11.01

Abstract

Recently, there are a great many research for magnetic levitation system. In case electromagnet is operated as the actuator of control system, first of all, we must analysis about an electromagnet. Important parameters of this system are inductance(L) and resistance(R) which are induced from the coil of electromagnet. And attractive force equation is also important. If the load of this system is large, phase delay is caused by self-inductance effect. Because this delay effect cause stability of whole magnetic evitation system to grow worse, a measures to diminish time constant must have been taken. And the linearized attractive force equation which is used at small range of the operating point is compensated to use at larger range, thus the experiment of magnetic levitation system will get a better result.

Keywords

References

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