Estimation and Control Under Information Constraints for LAAS Helicopter Benchmark

Author

Fradkov, Alexander L. ; Andrievsky, Boris ; Peaucelle, Dimitri

Author_Institution

Inst. of Problems in Mech. Eng., Russian Acad. of Sci., St. Petersburg, Russia

Volume

18

Issue

5

fYear

2010

Firstpage

1180

Lastpage

1187

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

adaptive control; continuous systems; discrete systems; helicopters; motion control; parameter estimation; state estimation; telecommunication channels; LAAS helicopter benchmark; adaptive tuning; coder range parameter; data transmission; helicopter pitch dynamic model; hybrid continuous discrete observation procedure; information constraint; limited band communication channel; parameter estimation; pitch motion Control; real time identification algorithm; state estimation; Benchmark testing; Channel capacity; Communication channels; Communication system control; Control systems; Helicopters; Laboratories; Motion control; Parameter estimation; State estimation; Helicopter control; information capacity; parameter identification; state estimation;

fLanguage

English

Journal_Title

Control Systems Technology, IEEE Transactions on

Publisher

ieee

ISSN

1063-6536

Type

jour

DOI

10.1109/TCST.2009.2033386

Filename

5291708