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Combined adaptive flight control system. / Abdrievsky, B. R.; Fradkov, A. L.

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

Research output: Contribution to journal › Conference article › peer-review

Harvard

Abdrievsky, BR & Fradkov, AL 2003, 'Combined adaptive flight control system', European Space Agency, (Special Publication) ESA SP, no. 516, pp. 299-302.

APA

Abdrievsky, B. R., & Fradkov, A. L. (2003). Combined adaptive flight control system. European Space Agency, (Special Publication) ESA SP, (516), 299-302.

Vancouver

Abdrievsky BR, Fradkov AL. Combined adaptive flight control system. European Space Agency, (Special Publication) ESA SP. 2003 Feb 1;(516):299-302.

Author

Abdrievsky, B. R. ; Fradkov, A. L. / Combined adaptive flight control system. In: European Space Agency, (Special Publication) ESA SP. 2003 ; No. 516. pp. 299-302.

BibTeX

@article{9415d0efa53740fb8583da09c6eeeaa2,
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.}",
year = "2003",
month = feb,
day = "1",
language = "English",
pages = "299--302",
journal = "European Space Agency, (Special Publication) ESA SP",
issn = "0379-6566",
publisher = "ESA Publication Division",
number = "516",
note = "5th ESA International Conference on Spacecraft Guidance, Navigation and Control Systems ; Conference date: 22-10-2002 Through 25-10-2002",

}

RIS

TY - JOUR

T1 - Combined adaptive flight control system

AU - Abdrievsky, B. R.

AU - Fradkov, A. L.

PY - 2003/2/1

Y1 - 2003/2/1

N2 - 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.

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.

UR - http://www.scopus.com/inward/record.url?scp=0038153039&partnerID=8YFLogxK

M3 - Conference article

AN - SCOPUS:0038153039

SP - 299

EP - 302

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

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

SN - 0379-6566

IS - 516

T2 - 5th ESA International Conference on Spacecraft Guidance, Navigation and Control Systems

Y2 - 22 October 2002 through 25 October 2002

ER -

ID: 37780719