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Target maneuvering estimation algorithm based on target motion characteristics analysis

  • Harbin Institute of Technology
  • Harbin Institute of Technology Weihai

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

Abstract

In this paper, the maneuvering target estimation algorithms is studied based on the near space hypersonic vehicle trajectory. Firstly, we analyze the possible maneuver forms. Basic description of typical target maneuvering scenarios is given such as cross range maneuver, longitudinal skip maneuver and terminal dive maneuver. Then, mathematical models of target maneuver estimation problems are obtained by combining the missile-target relative motion model and target maneuvering models. Moreover, this paper presents a target maneuvering estimation algorithm based on interacting multiple model with unscented Kalman filter (IMM-UKF). Finally, a simulation with different forms of target maneuvering is given to illustrate the effectiveness of the given filtering algorithm.

Original languageEnglish
Title of host publicationProceedings of the 35th Chinese Control Conference, CCC 2016
EditorsJie Chen, Qianchuan Zhao, Jie Chen
PublisherIEEE Computer Society
Pages5605-5610
Number of pages6
ISBN (Electronic)9789881563910
DOIs
StatePublished - 26 Aug 2016
Event35th Chinese Control Conference, CCC 2016 - Chengdu, China
Duration: 27 Jul 201629 Jul 2016

Publication series

NameChinese Control Conference, CCC
Volume2016-August
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference35th Chinese Control Conference, CCC 2016
Country/TerritoryChina
CityChengdu
Period27/07/1629/07/16

Keywords

  • Interacting Multiple Model
  • Near Space
  • Tracking
  • Unscented Kalman Filter

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