A fault-tolerant integrated navigation for UAV systems using time-variant vector distribution coefficients

  • Yueqian Liang*
  • , Yingmin Jia
  • , Fumitoshi Matsuno
  • *Corresponding author for this work

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

Abstract

The fault-tolerant integrated navigation is studied for the unmanned aerial vehicle (UAV) system. Considering different navigation accuracy and observability degree of each system state component, the vector distribution coefficients, which ensure the satisfaction of the law of conservation of information, are firstly developed for federated Kalman filter to get better navigation accuracy. Then, fault-tolerant navigation filters are proposed to detect and address the possible faults during the navigation period. Finally, aided by the relative bearing and speed information on the leader UAV, two navigation simulation examples are conducted to illustrate the effectiveness of the proposed method.

Original languageEnglish
Title of host publication2014 American Control Conference, ACC 2014
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages678-683
Number of pages6
ISBN (Print)9781479932726
DOIs
StatePublished - 2014
Event2014 American Control Conference, ACC 2014 - Portland, OR, United States
Duration: 4 Jun 20146 Jun 2014

Publication series

NameProceedings of the American Control Conference
ISSN (Print)0743-1619

Conference

Conference2014 American Control Conference, ACC 2014
Country/TerritoryUnited States
CityPortland, OR
Period4/06/146/06/14

Keywords

  • Fault-tolerant systems
  • Kalman filtering
  • Sensor fusion

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