Two designs are presented for control systems for the NASA Transport System Research Vehicle (TSRV) using integral Linear Quadratic Gaussian (LQG) methodology. The first is an integrated longitudinal autopilot/autothrottle design and the second design is an integrated lateral autopilot/yaw damper/sideslip controller design. It is shown that a systematic top-down approach to a complex design problem combined with proper application of modern control synthesis techniques yields a satisfactory solution in a reasonable period of time.


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    Titel :

    Design of Integrated Pitch Axis for Autopilot/Autothrottle and Integrated Lateral Axis for Autopilot/Yaw Damper for NASA TSRV (Transport System Research Vehicle) Airplane Using Integral LQG (Linear Quadratic Gaussian) Methodology


    Beteiligte:
    I. Kaminer (Autor:in) / R. A. Benson (Autor:in) / E. E. Coleman (Autor:in) / Y. S. Ebrahimi (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    152 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch