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권철현

Kwon, Cheolhyeon
High Assurance Mobility Control Lab.
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dc.citation.endPage 12568 -
dc.citation.number 5 -
dc.citation.startPage 12554 -
dc.citation.title IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS -
dc.citation.volume 61 -
dc.contributor.author Nam, Youngim -
dc.contributor.author Lee, Hojin -
dc.contributor.author Choi, Hyoekjin -
dc.contributor.author Ra, Won-Sang -
dc.contributor.author Kwon, Cheolhyeon -
dc.date.accessioned 2025-11-26T09:17:32Z -
dc.date.available 2025-11-26T09:17:32Z -
dc.date.created 2025-10-31 -
dc.date.issued 2025-10 -
dc.description.abstract This article proposes an attack intent inference framework for defending against hypersonic glide vehicles (HGVs). Predicting the HGV behaviors poses significant challenges for defense systems due to their highly dynamic and erratic maneuvers. Complementing the limitations of the dynamics model, a unified dynamics and decision-making model of HGV is developed. First, dynamically feasible attack regions can be set by the dynamics model. Within this region, the decision-making model encodes the rational intent of attack, strategically selecting the target that maximally attains the threat value. To further address the dynamical uncertainties and potential discrepancies from the rational decision-making model, a proximity parameter is introduced in light of the maximum entropy principle. The attack intent of the HGV is then inferred by the Bayesian approach, whereby recursively updates the probability of the potential target to be attacked. Numerical simulations demonstrate that the proposed framework achieves superior accuracy and faster convergence in intent inference compared to existing methods, under different scenarios with varying uncertainty levels. -
dc.identifier.bibliographicCitation IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.61, no.5, pp.12554 - 12568 -
dc.identifier.doi 10.1109/TAES.2025.3575052 -
dc.identifier.issn 0018-9251 -
dc.identifier.scopusid 2-s2.0-105007564375 -
dc.identifier.uri https://scholarworks.unist.ac.kr/handle/201301/88484 -
dc.identifier.wosid 001595002400017 -
dc.language 영어 -
dc.publisher IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC -
dc.title Attack Intent Inference of Hypersonic Glide Vehicle Based on a Unified Dynamics and Decision-Making Model -
dc.type Article -
dc.description.isOpenAccess FALSE -
dc.relation.journalWebOfScienceCategory Engineering, Aerospace; Engineering, Electrical & Electronic; Telecommunications -
dc.relation.journalResearchArea Engineering; Telecommunications -
dc.type.docType Article -
dc.description.journalRegisteredClass scie -
dc.description.journalRegisteredClass scopus -
dc.subject.keywordAuthor Decision making -
dc.subject.keywordAuthor Trajectory -
dc.subject.keywordAuthor Uncertainty -
dc.subject.keywordAuthor Heuristic algorithms -
dc.subject.keywordAuthor Prediction algorithms -
dc.subject.keywordAuthor Mathematical models -
dc.subject.keywordAuthor Inference algorithms -
dc.subject.keywordAuthor Numerical models -
dc.subject.keywordAuthor Vehicle dynamics -
dc.subject.keywordAuthor Aerodynamics -

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