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TsAGI Science Journal

ISSN Imprimir: 1948-2590
ISSN En Línea: 1948-2604

TsAGI Science Journal

DOI: 10.1615/TsAGISciJ.2018027659
pages 403-414

ESTIMATION OF THE LIMITING DEVIATIONS OF THE TRAJECTORY PARAMETERS OF AN AIRCRAFT DURING AUTOMATIC LANDING

Vasiliy Aleksandrovich Yaroshevsky
Central Aerohydrodynamic Institute (TsAGI) 1, Zhukovsky str., Zhukovsky, 140180, Moscow region, Russia
Viktor Petrovich Kuzmin

SINOPSIS

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.

REFERENCIAS

  1. Belogorodskyi, S.L., Automatization of Airplane Landing Control, Moscow: Transport, 1972 (in Russian).

  2. Ventsel’, E.S., The Probability Theory, Moscow: Nauka, 1958 (in Russian).

  3. Characteristics of wind perturbations in the low atmosphere layers, Obzor BnTI TsAGI, p. 545, 1979.

  4. Prudnikov, A.P., Brychkov, Yu.A., and Marichev, O.I., Integrals and Series, Moscow: Nauka, 1981 (in Russian).


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