The nonlinear aircraft motion and automatic control model is expanded to incorporate the human pilot into simulations of aircraft response to wind to wind shear. The human pilot is described by a constant gains lag filter. Two runs are carried out using pilot transfer functions. Fixed-stick, autopilot, and manned computer simulations are made with an aircraft having characteristics of a small commuter type aircraft flown through longitudinal winds measured by a Doppler radar beamed along the glide slope. Simulations are also made flying an aircraft through sinusoidal head wind and tail wind shears at the phugoid frequency to evaluate the response of manned aircraft in thunderstorm wind environments.


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    Titel :

    Pilot-Aircraft System Reponse to Wind Shear


    Beteiligte:
    B. S. Turkel (Autor:in) / W. Frost (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    98 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Pilot-aircraft system reponse to wind shear

    Turkel, B. S. / Frost, W. | NTRS | 1980


    Pilot-aircraft system response to wind shear

    TURKEL, B. / FROST, W. / CAMP, D.W. | AIAA | 1980


    Pilot-aircraft system response to wind shear

    Turkel, B. S. / Frost, W. / Camp, D. W. | NTRS | 1980


    Effects of Wind Shear on Aircraft: Low Level Wind Shear Alert System

    Rao, D. N. / Faizuddin, T. G. / Reddy, K. K. et al. | British Library Conference Proceedings | 1993


    Aircraft Flight in Wind-Shear

    D. Mclean | NTIS | 1990