GB/T 38997-2020General requirements for the flight control and navigation system of small and light multi-rotor unmanned aircraft (English PDF)

1 Scope

This standard specifies the general requirements and verification test for the flight control and navigation system of light and small multi-rotor drones (hereinafter referred to as “UAVs”).

Inspection and labeling, packaging, transportation and storage requirements.

This standard is applicable to the flight control and navigation system design of light and small multi-rotor drones (take-off weight between 0.25kg and 150kg).

Planning and manufacturing. Other UAV flight control and navigation systems can be implemented by reference.

2 Normative references

The following documents are indispensable for the application of this document. For dated reference documents, only the dated version applies to this article

Pieces. For undated references, the latest version (including all amendments) applies to this document.

GB/T 191 Packaging, storage and transportation pictorial signs

GB/T 4208-2017 Enclosure protection grade (IP code)

GB/T 9254-2008 Information Technology Equipment Radio Disturbance Limits and Measurement Methods

GB/T 17618-2015 Information Technology Equipment Immunity Limits and Measurement Methods

GB/T 35018 Classification and classification of civil unmanned aircraft systems

GB/T 38152 Unmanned Aircraft System Terminology

GB/T 38924.5 Environmental test method for civil light and small unmanned aerial vehicle systems Part 5.Impact test

GB/T 38924.6 Environmental test methods for civil light and small UAV systems Part 6.Vibration test

GB/T 38924.7 Environmental test method for civil light and small unmanned aerial vehicle system Part 7.Damp heat test

3 Terms, definitions and abbreviations