A multivariable synthesis procedure based on eigenvalue/eigenvector assignment is reviewed and is employed to develop a systematic design procedure to meet the lateral handling qualities design objectives of a fighter aircraft over a wide range of flight conditions. The closed loop modal characterization developed provides significant insight into the design process and plays a pivotal role in the synthesis of robust feedback systems. The simplicity of the synthesis algorithm yields an efficient computer aided interactive design tool for flight control system synthesis.


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    Titel :

    Modal control theory and application to aircraft lateral handling qualities design


    Beteiligte:

    Erscheinungsdatum :

    1978-06-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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