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

Seongjoong ParkDepartment of Aerospace Engineering, Seoul National University, Seoul, 08826, KoreaKi-Jun ByeonDepartment of Aerospace Engineering, Konkuk University, Seoul, 05029, KoreaYeonju ChoiDepartment of Aerospace Engineering, Konkuk University, Seoul, 05029, KoreaKwon-Su JeonKonkuk University Medical CenterMaxim TyanKonkuk Aerospace Design-Airworthiness Research Institute, Konkuk University, Seoul, 05029, KoreaSeok-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

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ABI

Annotatsiya

Annotatsiya mavjud emas.

Mavzular

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

Identifikatorlar

DOI: 10.1007/s42405-025-00927-5

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