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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2010, Vol. 31 ›› Issue (10): 1940-1945.

• Solid Mechanics and Vehicle Conceptual Design • Previous Articles     Next Articles

Multi-axis Vibration Control Research via Loop-shaping Design

Jiang Shuangyan, Chen Huaihai, He Xudong, You Weiqian   

  1. MOE Key Laboratory of Structure Mechanics and Control for Aircraft, Institute of Vibration Engineering Research, Nanjing University of Aeronautics and Astronautics
  • Received:2009-11-12 Revised:2010-03-30 Online:2010-10-25 Published:2010-10-25
  • Contact: Chen Huaihai

Abstract: In multi-exciter/multi-axis (MEMA) vibration control tests, it is frequently difficult for the auto-spectra of the control point responses to achieve the required reference targets at the frequency points where the frequency response function matrices are ill-conditioned. To cope with this problem, a new method is proposed in this article. The pre-compensator of the plant is obtained by curve fitting and modifying of the frequency response functions in a specified frequency range. The exciting spectrum matrix is then shaped via H loop-shaping theory. The shaped exciting matrix is used in the control loop computation instead of the original one. The experiment shows that the modified algorithm via loop-shaping design is capable of suppressing the adverse effect of the frequency response function at some specific frequencies. The auto-spectra of the control point responses are improved and become satisfactory.

Key words: loop-shaping design, multi-exciter/multi-axis, vibration test, vibration control, multi-input/multi-output

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