CONTROL OF FLUTTER IN BRIDGES

The suppression of the flutter instability of a suspension bridge by means of feedback control is studied. To this end, the mathematical model considered consists of the midsection of a bridge, assumed to be fixed at the bridge towers. The partial differential equations of motion can be converted into a set of second-order ordinary differential equations by using Galerkin's method. The design of optimal control is carried out by the independent modal-space control method. The closed-loop eigenvalues are selected so that the unstable flutter mode acquires a negative real part while the open-loop frequency remains unchanged. A numerical example is given in which the flutter of a suspension bridge deck having aerodynamic characteristics similar to those of the original Tacoma Narrows Bridge is controlled.

  • Availability:
  • Supplemental Notes:
    • Presented at the July 15-17, 1985, Second International Symposium on Structural Control, held at Waterloo, Canada.
  • Corporate Authors:

    American Society of Civil Engineers

    345 East 47th Street
    New York, NY  United States  10017-2398
  • Authors:
    • Meirovitch, L
    • GHOSH, D
  • Publication Date: 1987-5

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Filing Info

  • Accession Number: 00472570
  • Record Type: Publication
  • Report/Paper Numbers: Paper No. 21482
  • Files: TRIS
  • Created Date: Aug 31 1987 12:00AM