Fault-tolerant formation control of multiple UAVs in the presence of actuator faults

Summary In order to counteract actuator faults in formation flight of multiple unmanned aerial vehicles (UAVs), this paper presents a fault‐tolerant formation control (FTFC) design methodology, in which the reference generator and the finite‐time convergence of FTFC gains are explicitly considered....

Full description

Saved in:
Bibliographic Details
Published inInternational journal of robust and nonlinear control Vol. 26; no. 12; pp. 2668 - 2685
Main Authors Yu, Xiang, Liu, Zhixiang, Zhang, Youmin
Format Journal Article
LanguageEnglish
Published Bognor Regis Blackwell Publishing Ltd 01.08.2016
Wiley Subscription Services, Inc
Subjects
Online AccessGet full text

Cover

Loading…
More Information
Summary:Summary In order to counteract actuator faults in formation flight of multiple unmanned aerial vehicles (UAVs), this paper presents a fault‐tolerant formation control (FTFC) design methodology, in which the reference generator and the finite‐time convergence of FTFC gains are explicitly considered. Feasible references in response to actuator faults can be generated by considering the health and mission conditions of an overall team of UAVs. Moreover, by applying an auxiliary integrated regressor matrix and vector method, FTFC gains can converge within a finite amount of time to facilitate the fault accommodation process. Thus, the negative effects resulting from failed actuators can be compensated by the healthy/redundant actuators in UAVs. Simulation studies of UAV formation flight are carried out to exemplify the effectiveness of this design approach. Copyright © 2015 John Wiley & Sons, Ltd.
Bibliography:ArticleID:RNC3467
istex:3A164FB076F696555F0D6A2CC47B59A4441EC99C
ark:/67375/WNG-LC5RCHVB-Q
ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 14
content type line 23
ISSN:1049-8923
1099-1239
DOI:10.1002/rnc.3467