The ride quality experienced by passengers is a function of airframe rigid-body, elastic dynamic responses, autopilot, and stability augmentation system control inputs. A frequency response method has been developed to select sinusoidal elevator input time histories yielding vertical load factor distributions, within a given limit, as a function of fuselage station. The numerical technique is illustrated by applying two-degree-of-freedom short-period and first symmetric mode equations of motion to a B-1 aircraft at Mach 0.85 during sea level flight conditions.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Ride quality flight testing


    Beteiligte:
    Swaim, R. L. (Autor:in)


    Erscheinungsdatum :

    1978-04-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Ride Quality Flight Testing

    Robert L. Swaim | AIAA | 1978


    Ride-quality testing under controlled flight conditions

    SCHOONOVER, JR., W. / DITTENHAUSER, J. | AIAA | 1975


    Ride-quality testing under controlled flight conditions

    Schoonover, W. E., Jr. / Dittenhauser, J. | NTRS | 1975


    Flight research experiments on ride quality

    Jacobson, I. D. / Kuhlthau, A. R. | NTRS | 1975


    Flight Research Experiments on Ride Quality

    I. D. Jacobson / A. R. Kuhlthau | NTIS | 1975