Maximal admissible mode decision delay in terminal guidance

Shengwen XIANG, Tiancheng LI, Wei CHEN, Hongqi FAN, Qiang FU

Research output: Contribution to journalArticlepeer-review

1 Scopus citations

Abstract

Mode decision-maker is a critical component in the logic-based Integrated Estimation and Guidance (IEG) system. For the best possible estimation and guidance performance, the mode decision delay of the mode decision-maker should be limited to a range as small as possible. This paper presents a numerical method for computing the maximal admissible mode decision delay that varies with time-to-go. Particular attention has been paid to highly maneuvering target interception in terminal guidance. The results of this research offer useful guidelines for the design of the mode decision-maker in IEG systems.

Original languageEnglish
Pages (from-to)1959-1966
Number of pages8
JournalChinese Journal of Aeronautics
Volume32
Issue number8
DOIs
StatePublished - Aug 2019
Externally publishedYes

Keywords

  • Highly maneuvering target interception
  • Integrated Estimation and Guidance
  • Maximal admissible mode decision delay
  • Mode decision-maker
  • Numerical methods

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