A linearized translational rate system for near hover flight was optimized on a large motion simulator under the constraints of no disturbances and limited control power. Both lateral and longitudinal modes were considered with the primary variables of investigation being control sensitivity and response stiffness and secondarily system damping. Yaw and height control characteristics were represented by an angular rate and acceleration system, respectively. General regions of desired sensitivity and stiffness for the longitudinal and lateral modes were determined under VFR conditions for both the rapid maneuver task and the station keeping/mild maneuver task.


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    Titel :

    A VTOL translational rate control system study on a six degrees-of-freedom motion simulator


    Beteiligte:
    Corliss, L. D. (Autor:in) / Dugan, D. C. (Autor:in)

    Erscheinungsdatum :

    01.10.1972


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Use of a six-degrees-of-freedom motion simulator for VTOL hovering tasks

    Fry, E. B. / Gerdes, R. D. M. / Greif, R. K. | NTRS | 1969


    Use of a Six-Degrees-of-Freedom Motion Simulator for VTOL Hovering Tasks

    E. B. Fry / R. D. Gerdes / R. K. Greif | NTIS | 1969


    Use of a six-degrees-of-freedom motion simulator for VTOL hovering tasks

    Fry, Emmett B. / Greif, Richard K. / Gerdes, Ronald M. | TIBKAT | 1969


    VTOL control system studies on a six-degree- of-freedom motion simulator

    Fry, E. B. / Gerdes, R. M. / Gossett, T. D. et al. | NTRS | 1966


    VTOL control system studies on a six-degree- of-freedom motion simulator.

    Fry, E. B. / Gerdes, R. M. / Gossett, T. D. et al. | NTRS | 1967