An investigation was conducted to provide some insight into the importance of dynamic cross and cross-coupling derivatives in motion simulation studies of fighter aircraft in the maneuvering flight regime. The aircraft motion sensitivity to the various derivatives is ascertained in level and turning flight utilizing a 5 deg of freedom linearized stability program. The results are presented in a root locus format.


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    Titel :

    Aircraft Motion Sensitivity to Cross and Cross-Coupling Damping Derivatives


    Beteiligte:
    R. W. Butler (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    55 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







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