This standard specifies the general requirements, verification tests, marking, packaging, transportation and storage requirements for the flight control and navigation system of light and small multi-rotor unmanned aerial vehicles (hereinafter referred to as "UAVs"). This standard applies to the design and manufacturing of flight control and navigation systems for light and small multi-rotor UAVs (takeoff weight between 0.25kg and 150kg). Other UAV flight control and navigation systems can be implemented as a reference.
GB/T 38997-2020 Referenced Document
GB/T 17618-2015 Information technology equipment.Immunity characteristics.Limits and methods of measurement
GB/T 191 Packaging.Pictorial marking for handling of goods
GB/T 35018 Classification and grading for civil unmanned aircraft system
GB/T 38152 Terminology for unmanned aircraft system
GB/T 38924.5 Environmental test methods for civil small and light unmanned aircraft system—Part 5: Shock test
GB/T 38924.6 Environmental test methods for civil small and light unmanned aircraft system—Part 6: Vibration test
GB/T 38924.7 Environmental test methods for civil small and light unmanned aircraft system—Part 7: Humidity test
GB/T 4208-2017 Degrees of protection provide by enclosure (IP code)
GB/T 9254-2008 Information technology equipment - Radio disturbance characteristics - Limits and methods of measurement
GB/T 38997-2020 history
2020GB/T 38997-2020 General requirements for the flight control and navigation system of small and light multi-rotor unmanned aircraft