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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    Title :

    Aircraft Motion Sensitivity to Cross and Cross-Coupling Damping Derivatives


    Contributors:

    Publication date :

    1976


    Size :

    55 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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