The stability and control of a high-performance aircraft was analyzed, and a design methodology for a departure prevention stability augmentation system (DPSAS) was developed. A general linear aircraft model was derived which includes maneuvering flight effects and trim calculation procedures for investigating highly dynamic trajectories. The stability and control analysis systematically explored the effects of flight condition and angular motion, as well as the stability of typical air combat trajectories. The effects of configuration variation also were examined.


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    Title :

    Stability and Control of Maneuvering High-Performance Aircraft


    Contributors:
    R. F. Stengel (author) / P. W. Berry (author)

    Publication date :

    1977


    Size :

    206 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Stability and control of maneuvering high-performance aircraft

    Stengel, R. F. / Berry, P. W. | NTRS | 1976


    Stability and control of maneuvering high-performance aircraft

    Stengel, R. F. / Berry, P. W. | NTRS | 1977


    Stability and control of maneuvering high-performance aircraft

    Stengel, Robert F. / Berry, Paul W. | TIBKAT | 1977


    Stability and Control of Maneuvering High-Performance Aircraft

    Robert F. Stengel / Paul W. Berry | AIAA | 1977