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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    Title :

    IRAC Full-Scale Flight Testbed Capabilities


    Contributors:
    J. A. Lee (author) / J. Pahle (author) / B. R. Cogan (author) / C. E. Hanson (author) / J. T. Bosworth (author)

    Publication date :

    2009


    Size :

    17 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    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