A flight investigation was undertaken to study the problems associated with manual and automatic control of steep, decelerating instrument approaches and landings under simulated instrument conditions. The study was conducted with a research helicopter equipped with a three-cue flight-director indicator. The scope of the investigation included variations in the flight-director control laws, glide-path angle, deceleration profile, and control response characteristics. Investigation of the automatic-control problem resulted in the first automated approach and landing to a predetermined spot ever accomplished with a helicopter. Although well-controlled approaches and landings could be performed manually with the flight-director concept, pilot comments indicated the need for a better display which would more effectively integrate command and situation information.


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    Titel :

    Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings


    Beteiligte:
    Kelly, J. R. (Autor:in) / Niessen, F. R. (Autor:in) / Thibodeaux, J. J. (Autor:in) / Yenni, K. R. (Autor:in) / Garren, J. F., Jr. (Autor:in)

    Erscheinungsdatum :

    1974-07-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :