A flight research program was conducted to assess requirements for flightpath and airspeed control for glide-slope tracking during a precision approach and for flare control, particularly as applied to powered-lift, short takeoff and landing (STOL) aircraft. Ames Research Center's Augmentor Wing Research Aircraft was used to fly approaches on a 7.5 deg glide slope to landings on a 30 X 518 m (100 X 1700 ft) STOL runway. The dominant aircraft response characteristics determined were flightpath overshoot, flightpath-airspeed coupling, and initial flightpath response time. The significant contribution to control of the landing flare using pitch attitude was the short-term flightpath response. The limiting condition for initial flightpath response time for flare control with thrust was also identified. It is possible to define flying-qualities design criteria for glide-slope and flare control based on the aforementioned response characteristics.


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    Titel :

    Design criteria for flightpath and airspeed control for the approach and landing of STOL aircraft


    Beteiligte:
    Franklin, J. A. (Autor:in) / Innis, R. C. (Autor:in) / Hardy, G. H. (Autor:in) / Stephenson, J. D. (Autor:in)

    Erscheinungsdatum :

    1982-03-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch