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:

    Conference:

    NASA IRAC RFI Response Workshop ; 2009 ; Chicago, IL, United States


    Publication date :

    2009-08-09


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    IRAC Full-Scale Flight Testbed Capabilities

    J. A. Lee / J. Pahle / B. R. Cogan et al. | NTIS | 2009


    IRAC Full-scale Flight Test

    Bosworth, John T. | NTRS | 2008


    IRAC Full-scale Flight Test

    J. T. Bosworth | NTIS | 2008