November 02 (Thursday)
[CAE-동역학부문 Joint] 4차산업혁명(인공지능/머신러닝) (II)
Oral,
제12발표장(401A호),
09:50~10:50
  • Chair :
  •  전인기(브이피코리아)
Th12B-3
09:50~10:50
돌풍을 고려한 유연항공기 실시간 비행역학 해석기법
조맹효(서울대학교 공과대학), 김시호(서울대학교 기계항공공학부), 장성민(한국원자력연구원), 김의영(서울대학교)
This study presents the real-time analysis model for flexible aircraft flight dynamics considering gust effects. As the wing becomes slender, the larger deformation is generated which increases gust responses. To establish the framework for the flexible aircraft analysis, the aerodynamic model considering gust effects is developed using the structure model based on FFRF(Floating Frame of Reference Formulation). Based on this framework, then, the surrogate model is constructed using Neural Network training. The surrogate model enables the real-time analysis of flexible aircraft flight dynamics under the consideration of gust effects.
Keywords : Reduced Order Model for Real-time Flexible Aircraft Flight Dynamics considering Gust
Paper : Th12B-3.pdf

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