Design of variable structure guidance law for head-on interception based on variable coefficient strategy

Jun Hui Xiong*, Sheng Jing Tang, Jie Guo, Da Lin Zhu

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

11 Citations (Scopus)

Abstract

Head-on interception is a common guidance method for interception problem. The adaptive variable structure guidance law guiding the line-of-sight angular rate to converge to zero is available to improve the guidance precision. However, the variable structure guidance law leads to large required acceleration of interceptor before the line-of-sight angular rate converges to zero, especially in a situation where the target has strong maneuverability as well as high velocity. A strategy making the coefficients of the guidance law vary according to a typical rule via fuzzy control is proposed. Smaller guidance coefficients are selected at the beginning of terminal guidance. Therefore, the guidance command is reduced and a smaller acceleration of interceptor is incurred. As the coefficients grow to the fixed and desired values, the line-of-sight angular rate converges to zero rapidly so that the stability of the guidance system is guaranteed. It is concluded that the fuzzy variable coefficients strategy is highly effective for head-on interception as shown in the simulation.

Original languageEnglish
Pages (from-to)134-139
Number of pages6
JournalBinggong Xuebao/Acta Armamentarii
Volume35
Issue number1
DOIs
Publication statusPublished - Jan 2014

Keywords

  • Control and navigation technology of aerocraft
  • Fuzzy control
  • Head-on interception
  • Variable coefficient
  • Variable structure guidance law
  • Velocity ratio

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