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Control Technologies for Tailless Configurations in Sixth-Generation Fighter Aircraft

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dc.contributor.authorKim, Chongsup-
dc.contributor.authorKoh, Giok-
dc.contributor.authorChoi, Nagsun-
dc.contributor.authorHur, Gi-Bong-
dc.date.accessioned2025-11-10T08:30:11Z-
dc.date.available2025-11-10T08:30:11Z-
dc.date.issued2025-10-
dc.identifier.issn2093-274X-
dc.identifier.issn2093-2480-
dc.identifier.urihttps://scholarworks.gnu.ac.kr/handle/sw.gnu/80774-
dc.description.abstractSince the introduction of the Messerschmitt Me-262, developed by Germany in the early 1940s, fighter aircraft have undergone rapid advancements. Today, fifth-generation fighter aircraft, such as the F-22 Raptor, F-35 Lightning II, and Su-57 Felon, are operational in some nations, while major military powers, including the United States, Europe, and Russia, are actively pursuing the development of next-generation fighters. These aircraft are anticipated to feature extreme stealth configurations, such as tailless designs without vertical and horizontal stabilizers, alongside advanced technologies, including artificial intelligence, network-centric warfare, advanced sensor fusion, cloud-based data sharing, electronic warfare, high-performance propulsion systems, and directed energy weapon. With these advancements, next-generation fighters are expected to operate effectively in anti-access/area-denial environments, overcoming sophisticated integrated air defense system to achieve superior survivability and lethality on future battlefields. This paper reviews key control technologies for tailless aircraft, a critical design feature for achieving extreme stealth capabilities in future fighter platforms. The findings are expected to benefit a wide audience, from aerospace engineering students to industry researchers, by providing insights into the development goals of next-generation combat aircraft and the control technologies essential for tailless aircraft.-
dc.language영어-
dc.language.isoENG-
dc.publisherThe Korean Society for Aeronautical & Space Sciences-
dc.titleControl Technologies for Tailless Configurations in Sixth-Generation Fighter Aircraft-
dc.typeArticle-
dc.publisher.location대한민국-
dc.identifier.doi10.1007/s42405-025-01059-6-
dc.identifier.scopusid2-s2.0-105019766143-
dc.identifier.wosid001599736100001-
dc.identifier.bibliographicCitationInternational Journal of Aeronautical and Space Sciences-
dc.citation.titleInternational Journal of Aeronautical and Space Sciences-
dc.type.docTypeArticle; Early Access-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClassscie-
dc.description.journalRegisteredClassscopus-
dc.description.journalRegisteredClasskci-
dc.relation.journalResearchAreaEngineering-
dc.relation.journalWebOfScienceCategoryEngineering, Aerospace-
dc.subject.keywordPlusCONSTRAINED CONTROL ALLOCATION-
dc.subject.keywordPlusDYNAMIC CONTROL ALLOCATION-
dc.subject.keywordPlusRECONFIGURABLE FLIGHT-CONTROL-
dc.subject.keywordPlusNONLINEAR CONTROL ALLOCATION-
dc.subject.keywordPlusEIGENSTRUCTURE ASSIGNMENT-
dc.subject.keywordPlusFLOW-CONTROL-
dc.subject.keywordPlusCONTROL LAW-
dc.subject.keywordPlusDESIGN-
dc.subject.keywordPlusOPTIMIZATION-
dc.subject.keywordPlusALGORITHMS-
dc.subject.keywordAuthorKeyword-
dc.subject.keywordAuthorSixth-Generation Fighter Aircraft-
dc.subject.keywordAuthorControl Technologies-
dc.subject.keywordAuthorTailless Configurations-
dc.subject.keywordAuthorControl Allocation-
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