This report covers the flight test of a three-axis Hydrofluidic Stability Augmentation System (HYSAS) coupled with a completely independent parallel attitude and heading hold for a CH-54B helicopter. The design goal was to evaluate the performance of the CH-54B Automatic Flight Control System (AFCS) with the electronic SAS replaced with a fluidic SAS and to establish the technical base for a fluidic inner loop and electronic outer loop control system. (Modified author abstract)


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    Titel :

    Three-Axis Fluidic/Electronic Automatic Flight Control System Flight Test Report


    Beteiligte:
    L. S. Cotton (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    125 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch