每年出版 6 期
ISSN 打印: 1948-2590
ISSN 在线: 1948-2604
MATHEMATICAL MODEL OF THE AIRCRAFT AERODYNAMICS IN A VORTEX WAKE
摘要
The process of the generation and evolution of the vortex wake behind an aircraft in turbulent atmosphere is considered. An artificial neural networks–based approach to the development of a mathematical model of the aerodynamics of an aircraft during in-flight refueling is proposed. The accuracy and speed of the developed software module were evaluated for the problem of in-flight refueling modeling using a ground-based flight simulator.
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