Flight control actuators and feedback sensors suitable for use in a redundant digital flight control system were examined. The most appropriate design approach for an advanced digital flight control actuation system for development and use in a fly-by-wire system was selected. The concept which was selected consisted of a PM torque motor direct drive. The selected system is compatible with concurrent and independent development efforts on the computer system and the control law mechanizations.


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    Titel :

    Digital flight control actuation system study


    Beteiligte:
    Rossing, R. (Autor:in) / Hupp, R. (Autor:in)

    Erscheinungsdatum :

    1974-04-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Digital Flight Control Actuation System Study

    R. Rossing / R. Hupp | NTIS | 1974


    Digital Flight Control Actuation

    Escobosa, Alfonso | SAE Technical Papers | 1995


    Flight control actuation system

    Wingett, Paul T. / Gaines, Louie T. / Evans, Paul S. et al. | NTRS | 2006


    Flight control actuation system

    Wingett, Paul T. / Gaines, Louie T. / Evans, Paul S. et al. | NTRS | 2004


    Flight Control Actuation System

    P. T. Wingett / L. T. Gaines / P. S. Evans et al. | NTIS | 2004