A technique for obtaining a non-diagonal compensator for the control of a multi-input, multi-output plant is presented. The technique, which uses Quantitative Feedback Theory, provides guaranteed stability and performance robustness in the presence of parametric uncertainty. An example is given involving the lateral-directional control of an uncertain model of a high-performance fighter aircraft in which redundant control effectors are in evidence, i.e. more control effectors than output variables are used.


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    Title :

    QFT Multi-Input, Multi-Output Design with Non-Diagonal, Non-Square Compensation Matrices


    Contributors:

    Publication date :

    1996


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English