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. (Author)


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    Titel :

    Digital Flight Control Actuation System Study


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

    Erscheinungsdatum :

    1974


    Format / Umfang :

    490 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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