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    Optimal Output Feedback Control of Asymmetric Systems Using Complex Modes

    Source: Journal of Engineering for Gas Turbines and Power:;1993:;volume( 115 ):;issue: 002::page 307
    Author:
    G. W. Fan
    ,
    H. D. Nelson
    ,
    M. P. Mignolet
    DOI: 10.1115/1.2906710
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A Linear Quadratic Regulator (LQR)-based least-squares output feedback control procedure using a complex mode procedure is developed for the optimal vibration control of high-order asymmetric discrete system. An LQ Regulator is designed for a reduced-order model obtained by neglecting high-frequency complex modes of the original system. The matrix transformations between physical coordinates and complex mode coordinates are derived. The complex mode approach appears to provide more accurate reduced-order models than the normal mode approach for asymmetric discrete systems. The proposed least-squares output feedback control procedure takes advantage of the fact that a full-state feedback control is possible without using an observer. In addition, the lateral vibration of a high-order rotor system can be effectively controlled by monitoring one single location along the rotor shaft, i.e., the number of measured states can be much less than the number of eigenvectors retained in producing the reduced-order model while acceptable performance of the controller is maintained. The procedure is illustrated by means of a 52 degree-of-freedom finite element based rotordynamic system. Simulation results show that LQ regulators based on a reduced-order model with 12 retained eigenvalues can be accurately approximated by using feedback of four measured states from one location along the rotor shaft. The controlled and uncontrolled transient responses, using various numbers of measured states, of the original high-order system are shown. Comparisons of reduced-order model results using normal modes and complex modes are presented. The spillover problem is discussed for both collocated and noncollocated cases based on this same example.
    keyword(s): Feedback , Rotors , Discrete systems , Eigenvalues , Vibration , Control equipment , Transients (Dynamics) , Vibration control , Degrees of freedom , Finite element analysis AND Simulation results ,
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      Optimal Output Feedback Control of Asymmetric Systems Using Complex Modes

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/111933
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorG. W. Fan
    contributor authorH. D. Nelson
    contributor authorM. P. Mignolet
    date accessioned2017-05-08T23:41:19Z
    date available2017-05-08T23:41:19Z
    date copyrightApril, 1993
    date issued1993
    identifier issn1528-8919
    identifier otherJETPEZ-26715#307_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111933
    description abstractA Linear Quadratic Regulator (LQR)-based least-squares output feedback control procedure using a complex mode procedure is developed for the optimal vibration control of high-order asymmetric discrete system. An LQ Regulator is designed for a reduced-order model obtained by neglecting high-frequency complex modes of the original system. The matrix transformations between physical coordinates and complex mode coordinates are derived. The complex mode approach appears to provide more accurate reduced-order models than the normal mode approach for asymmetric discrete systems. The proposed least-squares output feedback control procedure takes advantage of the fact that a full-state feedback control is possible without using an observer. In addition, the lateral vibration of a high-order rotor system can be effectively controlled by monitoring one single location along the rotor shaft, i.e., the number of measured states can be much less than the number of eigenvectors retained in producing the reduced-order model while acceptable performance of the controller is maintained. The procedure is illustrated by means of a 52 degree-of-freedom finite element based rotordynamic system. Simulation results show that LQ regulators based on a reduced-order model with 12 retained eigenvalues can be accurately approximated by using feedback of four measured states from one location along the rotor shaft. The controlled and uncontrolled transient responses, using various numbers of measured states, of the original high-order system are shown. Comparisons of reduced-order model results using normal modes and complex modes are presented. The spillover problem is discussed for both collocated and noncollocated cases based on this same example.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOptimal Output Feedback Control of Asymmetric Systems Using Complex Modes
    typeJournal Paper
    journal volume115
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906710
    journal fristpage307
    journal lastpage313
    identifier eissn0742-4795
    keywordsFeedback
    keywordsRotors
    keywordsDiscrete systems
    keywordsEigenvalues
    keywordsVibration
    keywordsControl equipment
    keywordsTransients (Dynamics)
    keywordsVibration control
    keywordsDegrees of freedom
    keywordsFinite element analysis AND Simulation results
    treeJournal of Engineering for Gas Turbines and Power:;1993:;volume( 115 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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