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GB/T 38058-2019Test methods for civil multi-rotor unmanned aircraft system (English PDF)

民用多旋翼无人机系统试验方法

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Issued by

SAMR; SAC

Level / Type

National · Recommended

Issue date

October 18, 2019

Implementation date

May 1, 2020

Scope

GB/T 38058-2019 is the English-translated version of 民用多旋翼无人机系统试验方法.

GB/T 38058-2019 is the Chinese standard "Test methods for civil multi-rotor unmanned aircraft system". Its scope clause reads: This standard specifies the test methods for civil multi-rotor UAV systems and components.

This standard applies to civil light and small (maximum takeoff quality below 150kg) electric multi-rotor UAV system (hereinafter referred to as drone) Design, manufacture, testing and certification of systems and components; other types of UAV systems can also be implemented. Its clauses include terms and definitions.

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Document preview — GB/T 38058-2019

National Standard of the People's Republic of China

ICS: 49.020
Classification: V 35

Issued by: State Administration for Market Regulation; Standardization Administration of the PRC

Foreword
1 Scope
2 Normative references
3 Terms and Definitions
4 symbols and abbreviations
5 General
5.1 Test purpose
5.2 Test conditions and requirements
5.2.1 Technical Document
5.2.2 Tested product
5.2.3 Equipment and instrumentation
5.2.4 Personnel requirements
5.2.5 Management of the test article after entering the site
5.3 Test environment requirements
5.4 Test interruption and recovery
5.5 Qualification criteria
5.6 Test Outline
5.7 Test report
6 Test method
6.1 Test item
6.2 Basic inspection
6.2.1 Qiping
6.2.2 Appearance
6.2.3 Size
6.2.4 Quality and centroid
6.2.5 Institutional action
6.2.6 Connector
6.2.7 Filing registration
6.3 Function check
6.3.1 Identification
6.3.2 Route Binding
6.3.3 Self-detection
6.3.4 Comprehensive display
6.3.5 Data Storage
6.3.6 One-button return
6.3.7 Automatic obstacle avoidance
6.3.8 Typical Failure Protection
6.3.9 Takeoff and Landing
6.3.10 Alarm
6.3.11 Motor Locking and Startup
6.3.12 Control mode switching
6.4 Flight performance
6.4.1 Maximum takeoff quality
6.4.2 Maximum working radius
6.4.3 Maximum flight altitude
6.4.4 Maximum flying speed
6.4.5 Maximum climb rate
6.4.6 Height retention performance
6.4.7 Speed Maintenance Performance
6.4.8 Life time
6.4.9 Fixed hover
6.4.10 Positioning navigation
6.4.11 Track accuracy
6.4.12 Wind resistance
6.5 Battery System
6.5.1 Charging time
6.5.2 Discharge capacity
6.5.3 Battery cycle life
6.5.4 Working condition cycle life
6.5.5 Overcharge
6.5.6 Over discharge
6.5.7 Short circuit
6.5.8 Low pressure
6.5.9 Drop
6.5.10 Temperature cycle
6.5.11 Squeeze
6.5.12 Heat abuse
6.5.13 Soaking
6.6 Navigation system
6.6.1 Static attitude accuracy
6.6.2 Static Positioning Accuracy
6.7 Data Link System
6.7.1 Remote telemetry distance
6.7.2 Information transmission distance
6.7.3 Transmitter RF output power
6.7.4 Receiver sensitivity
6.7.5 Transmitter spurious emission power
6.7.6 Transmitter adjacent channel leakage ratio
6.7.7 Carrier Center Frequency
6.7.8 Receiver adjacent channel selectivity
6.8 Environmental adaptability
6.8.1 High temperature
6.8.2 Low temperature
6.8.3 Rain
6.8.4 Damp heat
6.8.5 Vibration
6.8.6 Impact
6.9 Electromagnetic Compatibility

1 Scope

This standard specifies the test methods for civil multi-rotor UAV systems and components.

This standard applies to civil light and small (maximum takeoff quality below 150kg) electric multi-rotor UAV system (hereinafter referred to as drone)

Design, manufacture, testing and certification of systems and components; other types of UAV systems can also be implemented.

2 Normative references

The following documents are indispensable for the application of this document. For dated references, only dated versions apply to this article.

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

GB/T 4208 enclosure protection grade (IP code)

GB/T 6113.101 Radio disturbance and immunity measuring equipment and measuring methods - Part 1-1. Radio disturbance and immunity

Measuring equipment measuring equipment

GB/T 6113.102 Radio disturbance and immunity measuring equipment and measuring methods - Part 1-2. Radio disturbance and immunity

Coupling device for measuring disturbance of conduction disturbance of equipment

GB/T 9254 Radio disturbance limits and methods of measurement for information technology equipment

GB/T 17626.1 Electromagnetic compatibility test and measurement technology immunity test

GB/T 17626.2 Electromagnetic compatibility test and measurement technology Electrostatic discharge immunity test

GB/T 17626.3 Electromagnetic compatibility test and measurement technology RF electromagnetic field radiation immunity test

GB/T 17626.4 Electromagnetic compatibility test and measurement technology Electrical fast transient burst immunity test

GB/T 17626.5 Electromagnetic compatibility test and measurement technology Surge (impact) immunity test

GB/T 17626.6 Electromagnetic compatibility test and measurement technology Conducted disturbance immunity of RF field induction

GB/T 17626.8 Electromagnetic compatibility test and measurement technology power frequency magnetic field immunity test

GB/T 17626.9 Electromagnetic compatibility test and measurement technology Pulse magnetic field immunity test

GB/T 17799.1 General standard for electromagnetic compatibility Immunity in residential, commercial and light industrial environments

GB/T 17799.2 Electromagnetic compatibility general standard immunity test in industrial environment

GB/T 17799.3 Electromagnetic compatibility common standards for emissions in residential, commercial and light industrial environments

GB/T 17799.4 Electromagnetic compatibility general standard emission in industrial environment

Aircraft airborne equipment -- Environmental conditions and test methods - Part 4. Damp heat test

3 Terms and definitions

The following terms and definitions apply to this document.

3.1 Task profile

A time-series description of the events and environments experienced by the product under test during the period in which the specified task is completed.

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This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — 25 pages — is available in the English PDF.

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