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Multi-objective Optimal Sizing Method for a Cruise Missile with Multi-phase Missions

Seongjoong ParkDepartment of Aerospace Engineering, Konkuk University, Seoul, 05029, KoreaKi-Jun ByeonDepartment of Aerospace Engineering, Konkuk University, Seoul, 05029, KoreaYeonju ChoiDepartment of Aerospace Engineering, Konkuk University, Seoul, 05029, KoreaKwon-Su JeonKonkuk Aerospace Design-Airworthiness Research Institute, Konkuk University, Seoul, 05029, KoreaMaxim TyanDepartment of Mechanical Engineering, New Uzbekistan University, Tashkent, UzbekistanSeok-Min ChoiLIG NEX1, Jukdong-Ro 181, Yu-Seong Gu, Daejeon, KoreaJae-Woo LeeDepartment of Aerospace Engineering, Konkuk University, Seoul, 05029, Korea

International Journal of Aeronautical and Space Sciencesjournal2025en

ABI

Аннотация

Аннотация мавжуд эмас.

Мавзулар

Guidance and Control Systems Aerospace Engineering and Control Systems Rocket and propulsion systems research

Идентификаторлар

DOI: 10.1007/s42405-025-00927-5

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