This poster presents the current adaptive control research being conducted at NASA ARC and LaRC in support of the Integrated Resilient Aircraft Control (IRAC) project. The technique 'Approximate Stability Margin Analysis of Hybrid Direct-Indirect Adaptive Control' has been developed at NASA ARC to address the needs for stability margin metrics for adaptive control that potentially enables future V&V of adaptive systems. The technique 'Direct Adaptive Control With Unknown Actuator Failures' is developed at NASA LaRC to deal with unknown actuator failures. The technique 'Adaptive Control with Adaptive Pilot Element' is being researched at NASA LaRC to investigate the effects of pilot interactions with adaptive flight control that can have implications of stability and performance.


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    Title :

    Adaptive Flight Control for Aircraft Safety Enhancements


    Contributors:
    N. T. Nguyen (author) / I. M. Gregory (author) / S. M. Joshi (author)

    Publication date :

    2008


    Size :

    1 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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