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Consensus of multiple flight vehicles in the presence of control input constraint

  • Harbin Institute of Technology

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

Abstract

Consensus problems for multiple flight vehicles with control input constraint is discussed in this paper. According to the characteristics of multiple flight vehicles salvo attack, problem of cooperative guidance is converted to the consensus of multiple flight vehicles. A cooperative guidance scheme based on consensus theory is proposed, which contains two key technologies. One is designed the normal acceleration command to ensure the convergence of the relative distance, another is develop the acceleration command along the line-of-sight (LOS) based on the finite time consensus theory, to ensure time-to-go of vehicles reach to consensus. Control input constraint is further considered, and process of prove the stability in this condition is given. Finally, simulation results of a three-to-one scenario show the proposed cooperative scheme can realize consensus of multiple flight vehicles.

Original languageEnglish
Title of host publicationCGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages695-700
Number of pages6
ISBN (Electronic)9781467383189
DOIs
StatePublished - 20 Jan 2017
Event7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016 - Nanjing, Jiangsu, China
Duration: 12 Aug 201614 Aug 2016

Publication series

NameCGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

Conference

Conference7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016
Country/TerritoryChina
CityNanjing, Jiangsu
Period12/08/1614/08/16

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