A piloted simulator was used to evaluate the flight path angle control capabilities of a system that employs spoiler direct lift control. The system was designated the velocity vector control system and was compared with a baseline flight path angle control system which used elevator for control. The simulated airplane was a medium jet transport. Research pilots flew a manual instrument landing system glide slope tracking task and a variable flight path angle task in the landing configuration to obtain comparative performance data.


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    Titel :

    Simulator evaluation of a flight-path-angle control system for a transport airplane with direct lift control


    Beteiligte:
    Kelley, W. W. (Autor:in)

    Erscheinungsdatum :

    01.03.1978


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch