Standard

Estimation and Control Under Information Constraints for LAAS Helicopter Benchmark. / Fradkov, Alexander L.; Andrievsky, Boris; Peaucelle, Dimitri.

In: IEEE Transactions on Control Systems Technology, Vol. 18, No. 5, 09.2010, p. 1180-1187.

Research output: Contribution to journal › Article › peer-review

Harvard

Fradkov, AL, Andrievsky, B & Peaucelle, D 2010, 'Estimation and Control Under Information Constraints for LAAS Helicopter Benchmark', IEEE Transactions on Control Systems Technology, vol. 18, no. 5, pp. 1180-1187. https://doi.org/10.1109/TCST.2009.2033386

APA

Fradkov, A. L., Andrievsky, B., & Peaucelle, D. (2010). Estimation and Control Under Information Constraints for LAAS Helicopter Benchmark. IEEE Transactions on Control Systems Technology, 18(5), 1180-1187. https://doi.org/10.1109/TCST.2009.2033386

Vancouver

Fradkov AL, Andrievsky B, Peaucelle D. Estimation and Control Under Information Constraints for LAAS Helicopter Benchmark. IEEE Transactions on Control Systems Technology. 2010 Sep;18(5):1180-1187. https://doi.org/10.1109/TCST.2009.2033386

Author

Fradkov, Alexander L. ; Andrievsky, Boris ; Peaucelle, Dimitri. / Estimation and Control Under Information Constraints for LAAS Helicopter Benchmark. In: IEEE Transactions on Control Systems Technology. 2010 ; Vol. 18, No. 5. pp. 1180-1187.

BibTeX

@article{f98f9a6e6c6348339fffa1ef5b89a143,
title = "Estimation and Control Under Information Constraints for LAAS Helicopter Benchmark",
abstract = "A scheme for state estimation and control under information constraints is implemented for {"}LAAS Helicopter benchmark{"}. Parameter estimates of the {"}Helicopter{"} pitch dynamics model are obtained by means of the real-time identification algorithm. The hybrid continuous-discrete observation procedure for transmission of the measured data over the limited-band communication channel with adaptive tuning of the coder range parameter is proposed and used in the experiments for pitch motion control of the {"}Helicopter{"}. Experimental results for pitch motion control of the {"}Helicopter{"} are presented, showing efficiency of the proposed method.",
keywords = "Helicopter control, information capacity, parameter identification, state estimation, FEEDBACK STABILIZATION, NONLINEAR-SYSTEMS, ADAPTIVE-CONTROL, DESIGN, SYNCHRONIZATION, STABILIZABILITY",
author = "Fradkov, {Alexander L.} and Boris Andrievsky and Dimitri Peaucelle",
year = "2010",
month = sep,
doi = "10.1109/TCST.2009.2033386",
language = "Английский",
volume = "18",
pages = "1180--1187",
journal = "IEEE Transactions on Control Systems Technology",
issn = "1063-6536",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
number = "5",

}

RIS

TY - JOUR

T1 - Estimation and Control Under Information Constraints for LAAS Helicopter Benchmark

AU - Fradkov, Alexander L.

AU - Andrievsky, Boris

AU - Peaucelle, Dimitri

PY - 2010/9

Y1 - 2010/9

N2 - A scheme for state estimation and control under information constraints is implemented for "LAAS Helicopter benchmark". Parameter estimates of the "Helicopter" pitch dynamics model are obtained by means of the real-time identification algorithm. The hybrid continuous-discrete observation procedure for transmission of the measured data over the limited-band communication channel with adaptive tuning of the coder range parameter is proposed and used in the experiments for pitch motion control of the "Helicopter". Experimental results for pitch motion control of the "Helicopter" are presented, showing efficiency of the proposed method.

AB - A scheme for state estimation and control under information constraints is implemented for "LAAS Helicopter benchmark". Parameter estimates of the "Helicopter" pitch dynamics model are obtained by means of the real-time identification algorithm. The hybrid continuous-discrete observation procedure for transmission of the measured data over the limited-band communication channel with adaptive tuning of the coder range parameter is proposed and used in the experiments for pitch motion control of the "Helicopter". Experimental results for pitch motion control of the "Helicopter" are presented, showing efficiency of the proposed method.

KW - Helicopter control

KW - information capacity

KW - parameter identification

KW - state estimation

KW - FEEDBACK STABILIZATION

KW - NONLINEAR-SYSTEMS

KW - ADAPTIVE-CONTROL

KW - DESIGN

KW - SYNCHRONIZATION

KW - STABILIZABILITY

U2 - 10.1109/TCST.2009.2033386

DO - 10.1109/TCST.2009.2033386

M3 - статья

VL - 18

SP - 1180

EP - 1187

JO - IEEE Transactions on Control Systems Technology

JF - IEEE Transactions on Control Systems Technology

SN - 1063-6536

IS - 5

ER -

ID: 76605301