Modeling and control of ACTEX distributed parameter system

Author

Khan, T. ; Yang, B. ; Wang, C.

Author_Institution

Dept. of Math., Univ. of Southern California, Los Angeles, CA, USA

Volume

4

fYear

2000

fDate

2000

Firstpage

2760

Abstract

We formulate a partial differential equation model for the ACTEX (advanced controls technology experiment) structure. The model takes the form of six one-dimensional Euler-Bernouilli beam equations. Two equations are used for each beam to model the transverse deformations in the local coordinates. Our model includes the passive and active contributions from the piezoceramic actuators and sensors in the internal and external bending moments. The results of the comparison of the ACTEX experimental data with simulation studies based upon our model are discussed

Keywords

aerospace control; distributed parameter systems; flexible structures; partial differential equations; piezoelectric actuators; piezoelectric transducers; vibration control; ACTEX; Euler-Bernouilli beam; advanced controls technology experiment; distributed parameter system; partial differential equation; piezoceramic actuators; piezoceramic sensors; vibration control; Accelerometers; Actuators; Distributed control; Distributed parameter systems; Equations; Mathematics; Satellites; Space technology; Thermostats; Transfer functions;

fLanguage

English

Publisher

ieee

Conference_Titel

American Control Conference, 2000. Proceedings of the 2000

Conference_Location

Chicago, IL

ISSN

0743-1619

Print_ISBN

0-7803-5519-9

Type

conf

DOI

10.1109/ACC.2000.878712

Filename

878712