DOI QR코드

DOI QR Code

입력성형기를 이용한 회전 유연보의 조종 및 진동제어

Maneuvering and Active Vibration Control of Slewing Flexible Beam Using Input Shaper

  • 곽문규 (동국대학교 기계로봇에너지공학과) ;
  • 양동호 (동국대학교 대학원) ;
  • 이재하 (동국대학교 대학원)
  • 투고 : 2012.03.14
  • 심사 : 2012.04.16
  • 발행 : 2012.06.20

초록

This research is concerned with the derivation of equations of motion for a slewing beam and the application of input shaper to the bang-bang control to achieve vibration suppression. When a uniform beam with a tip mass rotates about the axis perpendicular to the undeformed beam's longitudinal axis, it experiences inertial loading. Hence, the beam vibrates. In this paper, we used the input shaper for the maneuvering control to suppress vibrations. The maneuvering control which can achieve a minimum-time control is a bang-bang control. The input-shaped bang-bang maneuvering is used to suppress vibrations both theoretically and experimentally. The slewing beam experiment is not an easy subject because of the inherent damping existing inside the rotor. We propose the use of a negative damping to eliminate the rotor damping. Numerical and experimental results show that the input-shaper can be effectively used for the vibration suppression of a slewing beam.

키워드

참고문헌

  1. Garcia, E. and Inman, D. J., 1991, Modeling of the Slewing Control of a Flexible Structure, Journal of Guidance and Control, Vol. 14, No. 4, pp. 736-742. https://doi.org/10.2514/3.20707
  2. Denoyer, K. K. and Kwak, M. K., 1996, Dynamic Modeling and Vibration Suppression of a Slewing Structure Utilizing Piezoelectric Sensors and Actuators, Journal of Sound and Vibration, Vol. 189, No. 1, pp. 13-31. https://doi.org/10.1006/jsvi.1996.0003
  3. Kwak, M. K. and Nam, S. H., 2001, A Study on the Valid Dynamic Modeling for the Slewing and Vibration Suppression Control of Beam, Transactions of the Korean Society for Noise and Vibration Engineering. Vol. 11, No. 2, pp. 292-300.
  4. Singhose, W. E., Banerjee, A. K. and Seering, W., 1997, Slewing Flexible Spacecraft with Deflectionlimiting Input Shaping, Journal of Guidance, Control, and Dynamics, Vol. 21, No. 2, pp. 264-270.
  5. Gorinevsky, D. and Vukovich, G., 1998, Nonlinear Input Shaping Control of Flexible Spacecraft Reorientation Maneuver, Journal of Guidance, Control, and Dynamics, Vol. 21, No. 2, pp. 264-270. https://doi.org/10.2514/2.4252
  6. Yoo, H. H., Ryan, R. R. and Scott, R. A., 1995, Dynamics of Flexible Beams Undergoing Overall Motions, Journal of Sound and Vibration, Vol. 181, No. 2, pp. 261-278. https://doi.org/10.1006/jsvi.1995.0139
  7. Yun, S.-H., 2006, Formulations of Linear and Nonlinear Finite Element for Dynamic Flexible Beam, Journal of the Korean Society of Precision Engineering, Vol. 23, No. 2, pp. 113-121.
  8. Rusu, M. S., Grama, L. and Morar, A., 2009, Acta Electrotehnica, Vol. 50, No. 2, pp. 159-164.

피인용 문헌

  1. Vibration Control of Pendulum Using Input Shaping and Acceleration Feedback Controller vol.28, pp.6, 2018, https://doi.org/10.5050/KSNVE.2018.28.6.677