Результаты исследований: Научные публикации в периодических изданиях › Обзорная статья › Рецензирование
Обзор методов предотвращения раскачки самолета летчиком Светлой памяти Евгения Анатольевича Микрина посвящается. / Andrievsky, B.; Zaitseva, I. S.; Kudryashova, E. V.; Kuznetsov, N. V.; Kuznetsova, O. A.
в: Differencialnie Uravnenia i Protsesy Upravlenia, № 2, 2020, стр. 131-172.Результаты исследований: Научные публикации в периодических изданиях › Обзорная статья › Рецензирование
}
TY - JOUR
T1 - Обзор методов предотвращения раскачки самолета летчиком Светлой памяти Евгения Анатольевича Микрина посвящается
AU - Andrievsky, B.
AU - Zaitseva, I. S.
AU - Kudryashova, E. V.
AU - Kuznetsov, N. V.
AU - Kuznetsova, O. A.
N1 - Funding Information: Acknowledgements. This research is supported by Russian Science Foundation (project 19-41-02002, section 3) and by the Leading Scientific Schools of Russia (project NSh-2624.2020.1, sections 1–2). Publisher Copyright: © 2020 Saint-Petersburg State University. All rights reserved. Copyright: Copyright 2020 Elsevier B.V., All rights reserved.
PY - 2020
Y1 - 2020
N2 - The phenomenon of aircraft Pilot-Induced Oscillation (PIO) is well known from the very beginning of aviation development. It led to accidents and incidents in military aviation, and also served as a factor contributing to incidents and accidents in civil aviation. At the present stage, the problem of PIO is becoming increasingly important, affecting various classes of automated control systems, for example, such as remote control of drones, as well as spacecraft. This review attempts to characterize the phenomenon of PIO and give an idea of the available methods for its elimination. The article describes the PIO phenomenon and classifies its types, notes the connection between PIO and the technology of electric steering, presents the existing methods for preventing PIO, including organizational and technical measures for pilots training, conducting flight tests, and criteria for evaluating the aircraft flight quality. Particular attention is paid to algorithmic methods for PIO suppression implemented in the flight control system. Some numerical examples are presented.
AB - The phenomenon of aircraft Pilot-Induced Oscillation (PIO) is well known from the very beginning of aviation development. It led to accidents and incidents in military aviation, and also served as a factor contributing to incidents and accidents in civil aviation. At the present stage, the problem of PIO is becoming increasingly important, affecting various classes of automated control systems, for example, such as remote control of drones, as well as spacecraft. This review attempts to characterize the phenomenon of PIO and give an idea of the available methods for its elimination. The article describes the PIO phenomenon and classifies its types, notes the connection between PIO and the technology of electric steering, presents the existing methods for preventing PIO, including organizational and technical measures for pilots training, conducting flight tests, and criteria for evaluating the aircraft flight quality. Particular attention is paid to algorithmic methods for PIO suppression implemented in the flight control system. Some numerical examples are presented.
KW - Correction
KW - Nonlinear oscillations
KW - Pilot-induced oscillation
KW - Suppression
UR - http://www.scopus.com/inward/record.url?scp=85097623394&partnerID=8YFLogxK
M3 - Обзорная статья
AN - SCOPUS:85097623394
SP - 131
EP - 172
JO - ДИФФЕРЕНЦИАЛЬНЫЕ УРАВНЕНИЯ И ПРОЦЕССЫ УПРАВЛЕНИЯ
JF - ДИФФЕРЕНЦИАЛЬНЫЕ УРАВНЕНИЯ И ПРОЦЕССЫ УПРАВЛЕНИЯ
SN - 1817-2172
IS - 2
ER -
ID: 73410831