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Session: Aeroelastic testing 3
Session starts: Wednesday 19 June, 13:30
Presentation starts: 13:30
Room: Room 1.2

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Yi Liu (Institute of Beijing Mechanics and Electronics)
Kaihua Yuan (Institute of Beijing Mechanics and Electronics)
Xiaolong Cao (Institute of Beijing Mechanics and Electronics)
Yi Jin (Guangdong BODA Electronic Technology Co., Ltd)
Yang Meng (Beihang University)

Abstract:
Aeroelastic active control is an active and reasonable method to change the aerodynamic and structural characteristics of the aircraft by using structural deformation, which can enhance the stability control ability of the aircraft and improve the manoeuvrability and aerodynamic performance. The final aim is to reduce the structural response, expand the flight envelope, and improve the flight performance and flight safety. In this paper, the simulation and flight verification of active aeroelastic control technology are completed based on a flexible aeroelastic active control fight platform. The highest flight speed reached 200 km/h and the reduction of wing vibration is 30%, which laid a foundation for further application of aeroelastic active control technology to engineering model.