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Passification-based robust flight control system design. / Fradkov, Alexander L.; Andrievsky, Boris.

IFAC International Workshop on the Adaptation and Learning in Control and Signal Processing, ALCOSP 2010 - Proceedings. PART 1. ed. International Federation of Automatic Control, 2010. p. 66-71 (IFAC Proceedings Volumes (IFAC-PapersOnline); Vol. 1, No. PART 1).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review

Harvard

Fradkov, AL & Andrievsky, B 2010, Passification-based robust flight control system design. in IFAC International Workshop on the Adaptation and Learning in Control and Signal Processing, ALCOSP 2010 - Proceedings. PART 1 edn, IFAC Proceedings Volumes (IFAC-PapersOnline), no. PART 1, vol. 1, International Federation of Automatic Control, pp. 66-71, 10th IFAC International Workshop on Adaptation and Learning in Control and Signal Processing, ALCOSP 2010, Antalya, Turkey, 26/08/10. https://doi.org/10.3182/20100826-3-tr-4015.00015

APA

Fradkov, A. L., & Andrievsky, B. (2010). Passification-based robust flight control system design. In IFAC International Workshop on the Adaptation and Learning in Control and Signal Processing, ALCOSP 2010 - Proceedings (PART 1 ed., pp. 66-71). (IFAC Proceedings Volumes (IFAC-PapersOnline); Vol. 1, No. PART 1). International Federation of Automatic Control. https://doi.org/10.3182/20100826-3-tr-4015.00015

Vancouver

Fradkov AL, Andrievsky B. Passification-based robust flight control system design. In IFAC International Workshop on the Adaptation and Learning in Control and Signal Processing, ALCOSP 2010 - Proceedings. PART 1 ed. International Federation of Automatic Control. 2010. p. 66-71. (IFAC Proceedings Volumes (IFAC-PapersOnline); PART 1). https://doi.org/10.3182/20100826-3-tr-4015.00015

Author

Fradkov, Alexander L. ; Andrievsky, Boris. / Passification-based robust flight control system design. IFAC International Workshop on the Adaptation and Learning in Control and Signal Processing, ALCOSP 2010 - Proceedings. PART 1. ed. International Federation of Automatic Control, 2010. pp. 66-71 (IFAC Proceedings Volumes (IFAC-PapersOnline); PART 1).

BibTeX

@inproceedings{10b76dcb4bdd4c608bb6d88694eb2552,
title = "Passification-based robust flight control system design",
abstract = "A robust autopilot for attitude control of the flexible aircraft under parametric uncertainty is designed. The high gain controller with forced sliding motions is used to secure adaptability in the wide region of the aircraft model parameters. The shunting method is applied to ensure the closed-loop system stability in the face of the lack of the aircraft state information. The sequential reference model is used to assign the desired closed-loop system performance. An example illustrating a typical design procedure for aircraft attitude control in the horizontal plane for different flight conditions is given. The system robustness with respect to uncertain plant parameters is studied. The simulation results demonstrate efficiency and high robustness of the suggested control method.",
keywords = "Flight control, Robustness, Shunt compensation, Uncertain dynamic systems",
author = "Fradkov, {Alexander L.} and Boris Andrievsky",
note = "Funding Information: ★The work was supported by the Russian Foundation for Basic Research (Proj. Nos 08-01-00775, 09-08-00803), by the Russian Federal Program “Research and Teaching Cadres”, contract No 02.740.11.5056, and the Program of basic research of OEMPPU RAS No 2 “Control and safety in energy and technical systems”.; 10th IFAC International Workshop on Adaptation and Learning in Control and Signal Processing, ALCOSP 2010 ; Conference date: 26-08-2010 Through 28-08-2010",
year = "2010",
doi = "10.3182/20100826-3-tr-4015.00015",
language = "English",
isbn = "9783902661852",
series = "IFAC Proceedings Volumes (IFAC-PapersOnline)",
publisher = "International Federation of Automatic Control",
number = "PART 1",
pages = "66--71",
booktitle = "IFAC International Workshop on the Adaptation and Learning in Control and Signal Processing, ALCOSP 2010 - Proceedings",
address = "Austria",
edition = "PART 1",

}

RIS

TY - GEN

T1 - Passification-based robust flight control system design

AU - Fradkov, Alexander L.

AU - Andrievsky, Boris

N1 - Funding Information: ★The work was supported by the Russian Foundation for Basic Research (Proj. Nos 08-01-00775, 09-08-00803), by the Russian Federal Program “Research and Teaching Cadres”, contract No 02.740.11.5056, and the Program of basic research of OEMPPU RAS No 2 “Control and safety in energy and technical systems”.

PY - 2010

Y1 - 2010

N2 - A robust autopilot for attitude control of the flexible aircraft under parametric uncertainty is designed. The high gain controller with forced sliding motions is used to secure adaptability in the wide region of the aircraft model parameters. The shunting method is applied to ensure the closed-loop system stability in the face of the lack of the aircraft state information. The sequential reference model is used to assign the desired closed-loop system performance. An example illustrating a typical design procedure for aircraft attitude control in the horizontal plane for different flight conditions is given. The system robustness with respect to uncertain plant parameters is studied. The simulation results demonstrate efficiency and high robustness of the suggested control method.

AB - A robust autopilot for attitude control of the flexible aircraft under parametric uncertainty is designed. The high gain controller with forced sliding motions is used to secure adaptability in the wide region of the aircraft model parameters. The shunting method is applied to ensure the closed-loop system stability in the face of the lack of the aircraft state information. The sequential reference model is used to assign the desired closed-loop system performance. An example illustrating a typical design procedure for aircraft attitude control in the horizontal plane for different flight conditions is given. The system robustness with respect to uncertain plant parameters is studied. The simulation results demonstrate efficiency and high robustness of the suggested control method.

KW - Flight control

KW - Robustness

KW - Shunt compensation

KW - Uncertain dynamic systems

UR - http://www.scopus.com/inward/record.url?scp=84901921907&partnerID=8YFLogxK

U2 - 10.3182/20100826-3-tr-4015.00015

DO - 10.3182/20100826-3-tr-4015.00015

M3 - Conference contribution

AN - SCOPUS:84901921907

SN - 9783902661852

T3 - IFAC Proceedings Volumes (IFAC-PapersOnline)

SP - 66

EP - 71

BT - IFAC International Workshop on the Adaptation and Learning in Control and Signal Processing, ALCOSP 2010 - Proceedings

PB - International Federation of Automatic Control

T2 - 10th IFAC International Workshop on Adaptation and Learning in Control and Signal Processing, ALCOSP 2010

Y2 - 26 August 2010 through 28 August 2010

ER -

ID: 87375435