In this study in which an airplane simulator with one degree of freedom (pitch) was used, results were determined for three conditions of airplane dynamics. For an undamped natural frequency of 1/2 cps with a damping ratio of 0.18 and for an undamped natural frequency of 1 cps with a damping ratio of 0.11, moderate longitudinal stick forces and displacements were desired.


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    Title :

    Qualitative Simulator Study of Longitudinal Stick Forces and Displacements Desirable During Tracking


    Contributors:

    Publication date :

    1958-02-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English