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An Application Of Eigenspace Methods To Symmetric Flutter Suppression by Robert E. Fennell

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1DTIC ADA192758: An Application Of Eigenspace Methods To Symmetric Flutter Suppression.

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An eigenspace assignment approach to the design of parameter insensitive control laws for linear multivariable systems is presented. The control design scheme utilizes flexibility in eigenvector assignments to reduce control system sensitivity to changes in system parameters. The methods involve use of the singular value decomposition to provide an exact description of allowable eigenvectors in terms of a minimum number or design parameters. In a design example, the methods are applied to the problem of symmetric flutter suppression in an aeroelastic vehicle. In this example the flutter mode is sensitive to changes in dynamic pressure and eigenspace methods are used to enhance the performance of a stabilizing minimum energy/linear quadratic regulator controller and associated observer. Results indicate that the methods provide feedback control laws that make stability of the nominal closed loop systems insensitive to changes in dynamic pressure. Keywords: Stabilization; Eigenspace methods; Flutter suppression.

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  • Title: ➤  DTIC ADA192758: An Application Of Eigenspace Methods To Symmetric Flutter Suppression.
  • Author: ➤  
  • Language: English

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The book is available for download in "texts" format, the size of the file-s is: 18.30 Mbs, the file-s for this book were downloaded 48 times, the file-s went public at Sat Feb 17 2018.

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2NASA Technical Reports Server (NTRS) 19880008300: An Application Of Eigenspace Methods To Symmetric Flutter Suppression

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An eigenspace assignment approach to the design of parameter insensitive control laws for linear multivariable systems is presented. The control design scheme utilizes flexibility in eigenvector assignments to reduce control system sensitivity to changes in system parameters. The methods involve use of the singular value decomposition to provide an exact description of allowable eigenvectors in terms of a minimum number of design parameters. In a design example, the methods are applied to the problem of symmetric flutter suppression in an aeroelastic vehicle. In this example the flutter mode is sensitive to changes in dynamic pressure and eigenspace methods are used to enhance the performance of a stabilizing minimum energy/linear quadratic regulator controller and associated observer. Results indicate that the methods provide feedback control laws that make stability of the nominal closed loop systems insensitive to changes in dynamic pressure.

“NASA Technical Reports Server (NTRS) 19880008300: An Application Of Eigenspace Methods To Symmetric Flutter Suppression” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 19880008300: An Application Of Eigenspace Methods To Symmetric Flutter Suppression
  • Author: ➤  
  • Language: English

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The book is available for download in "texts" format, the size of the file-s is: 22.17 Mbs, the file-s for this book were downloaded 55 times, the file-s went public at Wed Sep 21 2016.

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