Significant performance improvements are possible through application of advanced flight control technology. This technology has been referred to as Control Configured Vehicles (CCV) and includes flutter mode control, ride smoothing, relaxed static stability (RSS) and maneuver load control (MLC). This study investigated the compatibility of two of these concepts, RSS and MLC. The primary question to be answered was: do the two concepts operating simultaneously enhance or degrade each other and are the combined performance gains the sum of the gains of the individual concepts. Two classes of military aircraft, a bomber and a fighter were used as a basis to determine if the compatibility was configuration dependent. (Author Modified Abstract)


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    Titel :

    Compatibility of Maneuver Load Control and Relaxed Static Stability


    Beteiligte:
    W. J. Rohling (Autor:in) / L. H. Pasley (Autor:in) / W. J. Wattman (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    125 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Compatibility of maneuver load control and relaxed static stability

    PASLEY, L. / ROHLING, W. / WATTMAN, W. | AIAA | 1973





    Modal control of relaxed static stability aircraft

    Rooney, R. H. / Chung, J. C. / Shapiro, E. Y. | NTRS | 1982