GB/T 38930-2020 Requirements and test methods of the capability of wind resistance for civil small and light unmanned aircraft system

Scope

This standard specifies the wind resistance requirements and test methods for civil small unmanned aerial vehicle systems, including wind resistance requirements, test purposes, test conditions, test environment, test interruption and recovery, test criteria, test process, test data processing, test result evaluation, and test reports. This standard applies to civil small rotary-wing UAV systems (with a takeoff weight of between 0.25 kg and 150 kg), including unmanned helicopter systems, multi-rotor UAV systems, vertical takeoff and landing fixed-wing UAV systems (during the takeoff and landing phases only), and other rotary-wing UAV systems; other types of UAV systems may refer to this standard for implementation.

Development Information

Referenced Standards

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