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ISSN Druckformat: 1948-2590
ISSN Online: 1948-2604
ESTIMATION OF THE LIMITING DEVIATIONS OF THE TRAJECTORY PARAMETERS OF AN AIRCRAFT DURING AUTOMATIC LANDING
ABSTRAKT
A method is proposed for specifying the worst longitudinal wind realizations during automatic aircraft flareout in order to estimate the limiting deviations of its trajectory parameters (i.e., vertical speed Vy and flight range L) corresponding to a small level of specified probability (Pspec = 10-5 to 10-7) at the moment the aircraft touches the runway. The proposed technique is used to study the automatic landing of a typical passenger aircraft.
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Ventsel’, E.S., The Probability Theory, Moscow: Nauka, 1958 (in Russian).
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Characteristics of wind perturbations in the low atmosphere layers, Obzor BnTI TsAGI, p. 545, 1979.
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Prudnikov, A.P., Brychkov, Yu.A., and Marichev, O.I., Integrals and Series, Moscow: Nauka, 1981 (in Russian).