Despite the application of sophisticated design methodology, newly introduced aircraft continue to suffer from basic flying qualities deficiencies. Two recent meetings, the DOD/NASA Workshop on Highly Augmented Aircraft Criteria and the NASA Dryden Flight Research Center/Air Force Flight Test Center/AIAA Pilot Induced Oscillation Workshop, addressed this problem. An overview of these meetings is provided from the point of view of the relationship between flying qualities criteria and flight control system design. Among the items discussed are flying qualities criteria development, the role of simulation, and communication between flying qualities specialists and control system designers.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Flying qualities criteria and flight control design


    Contributors:

    Conference:

    Guidance and Control Conference ; 1981 ; Albuquerque, NM


    Publication date :

    1981-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





    RPV flying qualities design criteria

    NEIGHBOR, T. / WILER, C. | AIAA | 1978



    Mission-specific flying qualities criteria

    Page, Mark / Gillette, Darrell | AIAA | 1994


    Longitudinal Flying Qualities Criteria for Single-Pilot Instrument Flight Operations

    Bar-Gill, Aharon / Stengel, Robert F. | SAE Technical Papers | 1983