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Evader maneuver on consideration of energy consumption in flight vehicle interception scenarios

  • Yang Guo*
  • , Shicheng Wang
  • , Yu Yao
  • , Baoqing Yang
  • *Corresponding author for this work
  • Harbin Institute of Technology
  • Xi'an Research Institute of High Technology

Research output: Contribution to journalArticlepeer-review

Abstract

To solve the problem of interception avoidance of flight vehicle, this paper comprehensively considers miss distance, energy consumption and prediction uncertainty on the final time of interception by a finite-time H∞ performance measure, and designs optimal energy consumption maneuver. An optimal interception against optimal evader maneuver of flight vehicle is also presented. The results show that the best evader effect will be achieved under condition of a large amplitude evader maneuver at the end of interception if the flight vehicle can predict the final time of interception accurately, and a large interception miss distance will be gained at a relatively small energy consumption.

Original languageEnglish
Pages (from-to)519-525
Number of pages7
JournalAerospace Science and Technology
Volume15
Issue number7
DOIs
StatePublished - Oct 2011

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

  1. SDG 7 - Affordable and Clean Energy
    SDG 7 Affordable and Clean Energy

Keywords

  • Finite-time
  • Missile interception
  • Optimal maneuver

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