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高超声速飞行器末段突防-打击均衡自适应 博弈制导

Translated title of the contribution: Adaptive Game Guidance with Balanced Penetration and Strike for Hypersonic Flight Vehicle in Terminal Phase
  • School of Astronautics, Harbin Institute of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

To address the contradictory requirements between terminal maneuver penetration and precision strike for hypersonic flight vehicles,a penetration-strike balanced adaptive game guidance method based on the minimum safe penetration boundary is proposed. Firstly,according to the minimum safe penetration distance constraint and combining the theories of game of kind and optimal control,an expected zero-effort miss boundary is established to ensure successful penetration and avoid excessive maneuvering,which provides a theoretical basis for the division of penetration and strike tasks. The three-party game among the flight vehicle,interceptor and target is decomposed into two independent two-player game problems for penetration and strike. Secondly,based on the mapping relationship between zero-effort miss and line-of-sight angular rate,a unified finite-horizon differential game model for penetration and strike is constructed with consideration of terminal state constraints,time constraints and energy optimization criteria. Furthermore,considering the difficulty of analytical solution,a single-Critic adaptive dynamic programming method is designed to online approximate and solve the Hamiltonian-Jacobi-Isaacs equation, so as to obtain near-optimal penetration and strike guidance commands. Simulation results demonstrate that the proposed method can guarantee penetration safety while ensuring terminal strike performance with approximately controllable penetration miss distance,and the terminal mission success rate reaches 94. 9%.

Translated title of the contributionAdaptive Game Guidance with Balanced Penetration and Strike for Hypersonic Flight Vehicle in Terminal Phase
Original languageChinese (Traditional)
Pages (from-to)1864-1879
Number of pages16
JournalYuhang Xuebao/Journal of Astronautics
Volume47
Issue number7
DOIs
StatePublished - Jul 2026
Externally publishedYes

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