Convergence-based analysis of robustness to delay in anti-windup loop of aircraft autopilot

Результат исследований: Научные публикации в периодических изданияхстатья в журнале по материалам конференции

6 Цитирования (Scopus)

Выдержка

The windup phenomenon is interpreted as a consequence of the convergent property absence for system with a saturation. This makes it possible to use the frequency-domain criterion for analysis of anti-windup augmentation in the case of stable and marginally stable plants. Based on this approach, robustness of the systems with respect to time delay in the anti-windup loop is examined and the approach for an optimal choice of the static anti-windup gain is proposed. An application of the convergence-based anti-windup control strategy to aircraft flight control for the case of time-delay in the anti-windup loop is described and studied by simulations.

Язык оригиналаанглийский
Страницы (с-по)144-149
Число страниц6
ЖурналIFAC-PapersOnLine
Том28
Номер выпуска9
DOI
СостояниеОпубликовано - 1 июл 2015
Событие1st IFAC Workshop on Advanced Control and Navigation for Autonomous Aerospace Vehicles, ACNAAV 2015 - Seville, Испания
Продолжительность: 10 июн 201512 июн 2015

Отпечаток

Time delay
Aircraft

Предметные области Scopus

  • Системотехника

Цитировать

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abstract = "The windup phenomenon is interpreted as a consequence of the convergent property absence for system with a saturation. This makes it possible to use the frequency-domain criterion for analysis of anti-windup augmentation in the case of stable and marginally stable plants. Based on this approach, robustness of the systems with respect to time delay in the anti-windup loop is examined and the approach for an optimal choice of the static anti-windup gain is proposed. An application of the convergence-based anti-windup control strategy to aircraft flight control for the case of time-delay in the anti-windup loop is described and studied by simulations.",
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Convergence-based analysis of robustness to delay in anti-windup loop of aircraft autopilot. / Andrievsky, Boris; Kuznetsov, Nikolay; Leonov, Gennady.

В: IFAC-PapersOnLine, Том 28, № 9, 01.07.2015, стр. 144-149.

Результат исследований: Научные публикации в периодических изданияхстатья в журнале по материалам конференции

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AU - Leonov, Gennady

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N2 - The windup phenomenon is interpreted as a consequence of the convergent property absence for system with a saturation. This makes it possible to use the frequency-domain criterion for analysis of anti-windup augmentation in the case of stable and marginally stable plants. Based on this approach, robustness of the systems with respect to time delay in the anti-windup loop is examined and the approach for an optimal choice of the static anti-windup gain is proposed. An application of the convergence-based anti-windup control strategy to aircraft flight control for the case of time-delay in the anti-windup loop is described and studied by simulations.

AB - The windup phenomenon is interpreted as a consequence of the convergent property absence for system with a saturation. This makes it possible to use the frequency-domain criterion for analysis of anti-windup augmentation in the case of stable and marginally stable plants. Based on this approach, robustness of the systems with respect to time delay in the anti-windup loop is examined and the approach for an optimal choice of the static anti-windup gain is proposed. An application of the convergence-based anti-windup control strategy to aircraft flight control for the case of time-delay in the anti-windup loop is described and studied by simulations.

KW - Anti-windup correction

KW - Convergent systems

KW - Flight control

KW - Integrator windup

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