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3. Метод нелінійної корекції перехідного процесу системи автоматичного наведення у режимі перекиду

Author

Kralina, I. V. and Belousov, B. N.

Subjects
nonlinear correction, нелінійна корекція, нелинейная коррекция, automatic guidance, автоматичне наведення, 681.3, автоматическое наведение
Abstract

Запропоновано і розглянуто алгоритм роботи системи автоматичного наведення з нелінійним коректуючим приладом, мінімізуючим час перехідного процесу перекиду до заданого напрямку. This is article work to describe the algorithm of a servo-mechanism work with nonlinear correcting device that has to minimize time of transient transfer in the specific direction that is considered. Предложен и рассмотрен алгоритм работы системы автоматического наведения в режиме переброса с нелинейным корректирующим устройством, минимизирующим время переходного процесса переброса в заданном направлении.

Published
2011

4. Boundary Problem of Supporting Surface in Nonstationary Limited Flow

Author

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO, Belousov,B N, Orishchenko,V I, FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO, Belousov,B N, and Orishchenko,V I

Abstract

Edited trans. of Materialy Konferentsii po Krayevym Zadacham, Izd vo Kazanskogo Universiteta (USSR) p36-41 1970, by Marilyn Olaechea.

Published
1977

5. Supporting Surface in Nonstationary Flow Near Screen

Author

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO, Belousov,B N, Lukashenko ,A N, Panchenkov,A N, FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO, Belousov,B N, Lukashenko ,A N, and Panchenkov,A N

Abstract

Edited trans. of Samoletostroyeniye i Tekhnika Vozdushnogo Flota, Kharkov (USSR) n18 p3-11 1970, by Marilyn Olaechea.

Published
1977

6. Lifting Surface in an Unsteady Flow Near a Screen (Nesushchaya Poverkhnost'v Nestatsionarnom Potoke Vblizi Ekrana)

Author

NAVAL INTELLIGENCE SUPPORT CENTER WASHINGTON D C TRANSLATION DIV, Belousov,B N, Lukashenko,A N, Panchenkov,A N, NAVAL INTELLIGENCE SUPPORT CENTER WASHINGTON D C TRANSLATION DIV, Belousov,B N, Lukashenko,A N, and Panchenkov,A N

Abstract

Several major works dealing with the theory of a lifting surface in an unsteady flow with various approximate methods of wing design are now in existence. It is common knowledge that the problem of a thin lifting surface of arbitrary aspect ratio is reduced to two-dimensional integral equations for which there are no closed solutions. One of the important aspects is the study of two-dimensional integral equations using one-dimensional approximations, and obtaining final results for the hydroaerodynamic characteristics of a wing in an unsteady flow on the basis of these equations., Trans. of Samoletostroveniye i Tekhnika Vozdushnogo Flota (USSR) n18 p3-11 1970.

Published
1976

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