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Adaptive control design and experiments for laas "helicopter" benchmark. / Fradkov, A. L.; Andrievsky, B.; Peaucelle, D.

в: European Journal of Control, Том 14, № 4, 2008, стр. 329-339.

Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование

Harvard

Fradkov, AL, Andrievsky, B & Peaucelle, D 2008, 'Adaptive control design and experiments for laas "helicopter" benchmark', European Journal of Control, Том. 14, № 4, стр. 329-339. https://doi.org/10.3166/ejc.14.329-339

APA

Fradkov, A. L., Andrievsky, B., & Peaucelle, D. (2008). Adaptive control design and experiments for laas "helicopter" benchmark. European Journal of Control, 14(4), 329-339. https://doi.org/10.3166/ejc.14.329-339

Vancouver

Fradkov AL, Andrievsky B, Peaucelle D. Adaptive control design and experiments for laas "helicopter" benchmark. European Journal of Control. 2008;14(4):329-339. https://doi.org/10.3166/ejc.14.329-339

Author

Fradkov, A. L. ; Andrievsky, B. ; Peaucelle, D. / Adaptive control design and experiments for laas "helicopter" benchmark. в: European Journal of Control. 2008 ; Том 14, № 4. стр. 329-339.

BibTeX

@article{1c22b2915fc54688b90934fdbf494dc8,
title = "Adaptive control design and experiments for laas {"}helicopter{"} benchmark",
abstract = "Application of the passification-based adaptive control technique for control of Quanser/LAAS {"}Helicopter{"} laboratory setup is presented. Two adaptive control laws for pitch angle control are designed and experimentally tested. The MATLAB/Simulink and WinCon software environment is used for adaptive control laws implementation and the real-world experiments. The experimental results demonstrate high closed loop system performance and robustness of the suggested control laws with respect to parametric uncertainties and unmodeled plant dynamics and actuator faults.",
keywords = "Adaptive control, Experimental results, Helicopter benchmark, Passification method",
author = "Fradkov, {A. L.} and B. Andrievsky and D. Peaucelle",
note = "Funding Information: This work was supported by the CNRS–RAS cooperative research program {\textquoteleft}{\textquoteleft}Robust and Adaptive Control of Complex Systems: Theory and Applications{\textquoteright}{\textquoteright} (project no. 19134), the Russian Foundation for Basic Research, project RFBR no. 06–08–01386, joint project RFBR–CNRS (PICS) no. 07–01–92166, and the Scientific Program of RAS no. 22 (project 1.8). The special thanks to the members of MAC group of LAAS–CNRS for the kind help in the work with the {\textquoteleft}{\textquoteleft}Helicopter{\textquoteright}{\textquoteright}.",
year = "2008",
doi = "10.3166/ejc.14.329-339",
language = "English",
volume = "14",
pages = "329--339",
journal = "European Journal of Control",
issn = "0947-3580",
publisher = "Lavoisier",
number = "4",

}

RIS

TY - JOUR

T1 - Adaptive control design and experiments for laas "helicopter" benchmark

AU - Fradkov, A. L.

AU - Andrievsky, B.

AU - Peaucelle, D.

N1 - Funding Information: This work was supported by the CNRS–RAS cooperative research program ‘‘Robust and Adaptive Control of Complex Systems: Theory and Applications’’ (project no. 19134), the Russian Foundation for Basic Research, project RFBR no. 06–08–01386, joint project RFBR–CNRS (PICS) no. 07–01–92166, and the Scientific Program of RAS no. 22 (project 1.8). The special thanks to the members of MAC group of LAAS–CNRS for the kind help in the work with the ‘‘Helicopter’’.

PY - 2008

Y1 - 2008

N2 - Application of the passification-based adaptive control technique for control of Quanser/LAAS "Helicopter" laboratory setup is presented. Two adaptive control laws for pitch angle control are designed and experimentally tested. The MATLAB/Simulink and WinCon software environment is used for adaptive control laws implementation and the real-world experiments. The experimental results demonstrate high closed loop system performance and robustness of the suggested control laws with respect to parametric uncertainties and unmodeled plant dynamics and actuator faults.

AB - Application of the passification-based adaptive control technique for control of Quanser/LAAS "Helicopter" laboratory setup is presented. Two adaptive control laws for pitch angle control are designed and experimentally tested. The MATLAB/Simulink and WinCon software environment is used for adaptive control laws implementation and the real-world experiments. The experimental results demonstrate high closed loop system performance and robustness of the suggested control laws with respect to parametric uncertainties and unmodeled plant dynamics and actuator faults.

KW - Adaptive control

KW - Experimental results

KW - Helicopter benchmark

KW - Passification method

UR - http://www.scopus.com/inward/record.url?scp=77954237162&partnerID=8YFLogxK

U2 - 10.3166/ejc.14.329-339

DO - 10.3166/ejc.14.329-339

M3 - Article

AN - SCOPUS:77954237162

VL - 14

SP - 329

EP - 339

JO - European Journal of Control

JF - European Journal of Control

SN - 0947-3580

IS - 4

ER -

ID: 87379673