Objectives: () Develop an asymmetric handling qualities metric to predict cross coupling effects of a damaged aircraft: (1) Initial use of U.S Army Aeronautical Design Specification ADS-33; (2) Modification as required based on flight test results. (b) Simulation and Flight Validation of proposed metric: (1) F-16 VISTA (March 2010); (2) F-18 Full Scale Test bed (Potential Early Experiment); and (3) Flight Simulators (GTM, ACFS, F-18 HILS). (c) Provide flight validated metric and tool box to control law designers.


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    Title :

    Flight Validation of a Handling Qualities Metric for a Damaged Aircraft


    Contributors:
    B. R. Cogan (author)

    Publication date :

    2009


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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