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Finite-time H2 performance measure-based strategy design

  • Yang Guo*
  • , Yu Yao
  • , Shi Cheng Wang
  • , Feng Hua He
  • *Corresponding author for this work
  • Harbin Institute of Technology
  • Xi'an Research Institute of High Technology

Research output: Contribution to journalArticlepeer-review

Abstract

Based on finite-time H2 performance measure, a criterion of analysis and design is given and a type of optimal maneuver is designed in consideration of both energy cost and miss distance. In the light of an interceptor guidance law with uncertainties, a method of finite-time robust H2 performance analysis and a guaranteed cost control criterion are derived, and the guaranteed performance maneuver is designed under the condition of interceptor guidance law with uncertainty. The results show that a substantial maneuvering near the end of penetration process is most effective, and able to cause large miss distance by minimum energy consumption.

Original languageEnglish
Pages (from-to)2289-2294
Number of pages6
JournalYuhang Xuebao/Journal of Astronautics
Volume31
Issue number10
DOIs
StatePublished - Oct 2010

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
  • Guaranteed cost control
  • H control
  • Maneuvering

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