Back-stepping sliding mode control for missile systems via quaternions

Zheng Zhu*, Yuanqing Xia, Mengyin Fu

*Corresponding author for this work

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

3 Citations (Scopus)

Abstract

A novel approach combining the sliding mode control and extended state observer is proposed for attitude control of a quaternion missile model which is nonlinear in aerodynamics. Combining the back-stepping technique, the corresponding sliding mode controller is designed to guarantee the state variables of the closed loop system to converge to the reference state with the help of the extended state observer by estimating the uncertainties. Also, simulation results are presented to illustrate the effectiveness of the control strategy.

Original languageEnglish
Title of host publicationProceedings of the 48th IEEE Conference on Decision and Control held jointly with 2009 28th Chinese Control Conference, CDC/CCC 2009
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages6089-6094
Number of pages6
ISBN (Print)9781424438716
DOIs
Publication statusPublished - 2009
Event48th IEEE Conference on Decision and Control held jointly with 2009 28th Chinese Control Conference, CDC/CCC 2009 - Shanghai, China
Duration: 15 Dec 200918 Dec 2009

Publication series

NameProceedings of the IEEE Conference on Decision and Control
ISSN (Print)0743-1546
ISSN (Electronic)2576-2370

Conference

Conference48th IEEE Conference on Decision and Control held jointly with 2009 28th Chinese Control Conference, CDC/CCC 2009
Country/TerritoryChina
CityShanghai
Period15/12/0918/12/09

Fingerprint

Dive into the research topics of 'Back-stepping sliding mode control for missile systems via quaternions'. Together they form a unique fingerprint.

Cite this