Combined adaptive flight control system

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

8 Цитирования (Scopus)

Выдержка

Combined adaptive control scheme is presented and used for adaptive control for attitude of the aircraft with uncertain parameters. The proposed controller ensures finite time convergence of augmented error omitting to relay term in control law and exponential convergence of the parameter error under the condition of persistent excitation. This allows achieving the desired dynamics to the true plant output. The simulation results demonstrate high adaptability properties of the proposed controller.

Язык оригиналаанглийский
Страницы (с-по)299-302
Число страниц4
ЖурналEuropean Space Agency, (Special Publication) ESA SP
Номер выпуска516
СостояниеОпубликовано - 1 фев 2003
Событие5th ESA International Conference on Spacecraft Guidance, Navigation and Control Systems - Frascati, Италия
Продолжительность: 22 окт 200225 окт 2002

Отпечаток

flight control
Adaptive control systems
Flight control systems
adaptive control
control system
controllers
flight
relay
aircraft
Controllers
output
Aircraft
excitation
simulation
parameter

Предметные области Scopus

  • Авиакосмическая техника

Цитировать

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title = "Combined adaptive flight control system",
abstract = "Combined adaptive control scheme is presented and used for adaptive control for attitude of the aircraft with uncertain parameters. The proposed controller ensures finite time convergence of augmented error omitting to relay term in control law and exponential convergence of the parameter error under the condition of persistent excitation. This allows achieving the desired dynamics to the true plant output. The simulation results demonstrate high adaptability properties of the proposed controller.",
author = "Abdrievsky, {B. R.} and Fradkov, {A. L.}",
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Combined adaptive flight control system. / Abdrievsky, B. R.; Fradkov, A. L.

В: European Space Agency, (Special Publication) ESA SP, № 516, 01.02.2003, стр. 299-302.

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

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AB - Combined adaptive control scheme is presented and used for adaptive control for attitude of the aircraft with uncertain parameters. The proposed controller ensures finite time convergence of augmented error omitting to relay term in control law and exponential convergence of the parameter error under the condition of persistent excitation. This allows achieving the desired dynamics to the true plant output. The simulation results demonstrate high adaptability properties of the proposed controller.

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JO - European Space Agency, (Special Publication) ESA SP

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