Skip to main navigation Skip to search Skip to main content

Composite disturbance-observer-based control and terminal sliding mode control for uncertain structu

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

A new type of composite control scheme of disturbance-observer-based control and terminal sliding mode control is proposed for uncertain structural systems. The disturbance are supposed to include two parts. One is generated by an exogenous system, which can represent the harmonic signals with modeling perturbations in structural system. The other part is external excitation in H2-norm context. By combining the disturbance observer with terminal sliding mode control law, the disturbance with the exogenous system can be estimated and compensated, and external excitation can be attenuated in finite time which can be computed by our approach. Especially,the design of disturbance observer and controller can be obtained separately. Finally, simulations for a four-degree-of-freedom building model excited by 1940 El Centro earthquake excitation are given to demonstrate the effectiveness of the approach and compare the proposed results with the previous schemes in accuracy.

Original languageEnglish
Title of host publicationProceedings of the 17th World Congress, International Federation of Automatic Control, IFAC
Edition1 PART 1
DOIs
StatePublished - 2008
Event17th World Congress, International Federation of Automatic Control, IFAC - Seoul, Korea, Republic of
Duration: 6 Jul 200811 Jul 2008

Publication series

NameIFAC Proceedings Volumes (IFAC-PapersOnline)
Number1 PART 1
Volume17
ISSN (Print)1474-6670

Conference

Conference17th World Congress, International Federation of Automatic Control, IFAC
Country/TerritoryKorea, Republic of
CitySeoul
Period6/07/0811/07/08

Keywords

  • Disturbance rejection
  • Nonlinear observer and filter design
  • Nonlinear system control

Fingerprint

Dive into the research topics of 'Composite disturbance-observer-based control and terminal sliding mode control for uncertain structu'. Together they form a unique fingerprint.

Cite this