1、 Scope of application

Suitable for wind resistance performance testing of civil light and small rotary wing unmanned aerial vehicles (with takeoff weight between 0.25 kg and 150 kg), capable of simulating different

To study the flight status of aircraft under different complex wind speeds and turbulence levels, including the wind speed state and dynamic fluid wind field under different wind speed arrays.

2、 According to the standard

GB 42590-2023 "Safety Requirements for Civil Unmanned Aerial Vehicle Systems";

GB/T38930-2020 "Wind resistance requirements and test methods for civil light and small unmanned aerial vehicle systems";

GB/T 38058-2019 "Test Methods for Civil Multi rotor Unmanned Aerial Vehicle Systems".