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A novel mid-course doctrine for multiple flight vehicles cooperative interception

  • Long Wang*
  • , Yu Yao
  • , Fenghua He
  • , Kai Liu
  • *Corresponding author for this work
  • Harbin Institute of Technology
  • Beijing Aerospace Technology Institute

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

Abstract

In this paper, we consider the problem of intercepting a target with large information uncertainties during the mid-course guidance, which will result in a large inertial error of the terminal guidance. In order to improve the interception probability, multiple intercepting flight vehicles are employed. Taking the information transmission between the flight vehicles into consideration, a novel cooperative doctrine for mid-course guidance is proposed to guarantee the interception probability with fewer intercepting flight vehicles. Then in order to maximize the interception probability of the target, an optimization problem is established to design the optimal relative motion parameters between the flight vehicle and target at the handover moment, as well as the optimal interval between the handover time of different flight vehicles. A preliminary approach is proposed and simulation experiments are carried out to show the feasibility of the proposed cooperative doctrine.

Original languageEnglish
Title of host publicationCGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages252-257
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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