Overview: Provide validation of adaptive control law concepts through full scale flight evaluation in a representative avionics architecture. Develop an understanding of aircraft dynamics of current vehicles in damaged and upset conditions Real-world conditions include: a) Turbulence, sensor noise, feedback biases; and b) Coupling between pilot and adaptive system. Simulated damage includes 1) 'B' matrix (surface) failures; and 2) 'A' matrix failures. Evaluate robustness of control systems to anticipated and unanticipated failures.


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    Titel :

    IRAC Full-Scale Flight Testbed Capabilities


    Beteiligte:
    J. A. Lee (Autor:in) / J. Pahle (Autor:in) / B. R. Cogan (Autor:in) / C. E. Hanson (Autor:in) / J. T. Bosworth (Autor:in)

    Erscheinungsdatum :

    2009


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    IRAC Full-Scale Flight Testbed Capabilities

    Lee, James A. / Pahle, Joseph / Cogan, Bruce R. et al. | NTRS | 2009


    IRAC Full-scale Flight Test

    Bosworth, John T. | NTRS | 2008


    IRAC Full-scale Flight Test

    J. T. Bosworth | NTIS | 2008