Доступ предоставлен для: Guest
TsAGI Science Journal

Выходит 6 номеров в год

ISSN Печать: 1948-2590

ISSN Онлайн: 1948-2604

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

Том 49, Выпуск 4, 2018, pp. 403-414
DOI: 10.1615/TsAGISciJ.2018027659
Get accessGet access

Краткое описание

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.

ЛИТЕРАТУРА
  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).

Последний выпуск

KIRILL IVANOVICH SYPALO−50TH ANNIVERSARY NUMERICAL STUDY OF THE DISTURBANCES GENERATED BY MICROJETS IN A SUPERSONIC FLAT-PLATE BOUNDARY LAYER Andrei Valerievich Novikov, Alexander Vitalyevich Fedorov, Ivan Vladimirovich Egorov, Anton Olegovich Obraz, Nikolay Nikolaevich Semenov ANALYSIS OF THE MOVING DETONATION INTERACTION WITH TURBULENT BOUNDARY LAYERS IN A DUCT ON THE BASIS OF NUMERICAL SIMULATION Vladimir Anatolievich Sabelnikov, Vladimir Viktorovich Vlasenko, Sergey Sergeyevich Molev EXPERIMENTAL STUDY OF COUNTERFLOW BLOWING IN HIGH-SPEED FLOW THROUGH AN ASYMMETRIC SLOT IN THE LEADING EDGE OF A SHARP WEDGE Eduard Borisovich Vasilevskii, Ivan Valeryevich Ezhov, Pavel Vladimirovich Chuvakhov ASYMPTOTIC SOLUTIONS TO HYPERSONIC BOUNDARY LAYER EQUATIONS ON A FLAT WING WITH A POINT OF INFLECTION ON THE LEADING EDGE Georgiy Nikolaevich Dudin, Aleksey Vyacheslavovich Ledovskiy WAVE MODEL OF ORGANIZED STRUCTURES IN A TURBULENT BOUNDARY LAYER ON A PLATE WITH ZERO LONGITUDINAL PRESSURE GRADIENT Vladimir Alekseevich Zharov, Igor Ivanovich Lipatov, Rami Salah Saber Selim NUMERICAL SIMULATION OF THE FLOW AROUND LANDSCAPE FRAGMENTS AND SOLUTION VERIFICATION Viktor Viktorovich Vyshinsky, Koang T'in' Zoan POLYNOMIAL REPRESENTATION OF THERMODYNAMIC PROPERTIES OF COMBINED FUEL SYSTEMS IN RAMJET SIMULATION MODELS Timur Romanovich Zuev, Mikhail Semenovich Tararyshkin A MODEL TEST METHODOLOGY FOR THE INVESTIGATION OF AN ELASTICALLY SCALED MAIN ROTOR Maxim Andreyevich Ledyankin , Sergey Anatolyevich Mikhailov, Dmitry Valeryevich Nedel'ko, Timur Arturovich Agliullin INDEX, VOLUME 51, 2020
Портал Begell Электронная Бибилиотека e-Книги Журналы Справочники и Сборники статей Коллекции Цены и условия подписки Begell House Контакты Language English 中文 Русский Português German French Spain