A broad research program to identify maneuvering requirements for advanced fighters and the corresponding design criteria to aid in making critical design tradeoffs is being conducted under the NASA High-Angle-of-Attack Technology Program (HATP). As part of this activity, NASA and the U.S. Navy are conducting cooperative research to develop high-angle-of-attack control margin requirements. This paper will summarize the status of this program. Following some background information, the simulation study conducted to develop a set of preliminary guidelines for nose-down pitch control is reviewed, and the results of some very limited flight tests are described.


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    Title :

    Development of High-Angle-of-Attack Nose-down Pitch Control Margin Design Guidelines for Combat Aircraft


    Contributors:
    M. E. Ogburn (author) / J. V. Foster (author)

    Publication date :

    1993


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Development of High-Angle-of-Attack Nose-Down Pitch Control Margin Design Guidelines for Combat Aircraft

    Ogburn, M. E. / United States / National Aeronautics and Space Administration| Langley Research Center | British Library Conference Proceedings | 1994



    Status of the Validation of High-Angle-Of-Attack Nose-Down Pitch Control Margin Design Guidelines

    Ogburn, Marilyn E. / Foster, John V. / Pahle, Joseph W. et al. | NTRS | 1992


    Status of the validation of high-angle-of-attack nose-down pitch control margin design guidelines

    OGBURN, MARILYN / FOSTER, JOHN / PAHLE, JOSEPH et al. | AIAA | 1993