GB/T 38058-2019 English PDF

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GB/T 38058-2019: Test methods for civil multi-rotor unmanned aircraft system
Status: Valid

Standard ID	USD	BUY PDF	Lead-Days	Standard Title (Description)	Status
GB/T 38058-2019	679	Add to Cart	6 days	Test methods for civil multi-rotor unmanned aircraft system	Valid

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Basic data

Standard ID: GB/T 38058-2019 (GB/T38058-2019)
Description (Translated English): Test methods for civil multi-rotor unmanned aircraft system
Sector / Industry: National Standard (Recommended)
Classification of Chinese Standard: V35
Classification of International Standard: 49.020
Word Count Estimation: 34,384
Date of Issue: 2019-10-18
Date of Implementation: 2020-05-01
Issuing agency(ies): State Administration for Market Regulation, China National Standardization Administration

GB/T 38058-2019: Test methods for civil multi-rotor unmanned aircraft system

---This is a DRAFT version for illustration, not a final translation. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.) will be manually/carefully translated upon your order.
Test methods for civil multi-rotor unmanned aircraft system ICS 49.020 V35 National Standards of People's Republic of China Civil multi-rotor UAV system test method Published on.2019-10-18 2020-05-01 implementation State market supervision and administration China National Standardization Administration issued

Content

Foreword III 1 Scope 1 2 Normative references 1 3 Terms and Definitions 1 4 symbols and abbreviations 2 5 General 2 5.1 Test purpose 2 5.2 Test conditions and requirements 2 5.2.1 Technical Document 2 5.2.2 Tested product 2 5.2.3 Equipment and instrumentation 2 5.2.4 Personnel requirements 2 5.2.5 Management of the test article after entering the site 3 5.3 Test environment requirements 3 5.4 Test interruption and recovery 3 5.5 Qualification criteria 3 5.6 Test Outline 3 5.7 Test report 4 6 Test method 4 6.1 Test item 4 6.2 Basic inspection 6 6.2.1 Qiping 6 6.2.2 Appearance 6 6.2.3 Size 6 6.2.4 Quality and centroid 6 6.2.5 Institutional action 7 6.2.6 Connector 7 6.2.7 Filing registration 7 6.3 Function check 7 6.3.1 Identification 7 6.3.2 Route Binding 7 6.3.3 Self-detection 7 6.3.4 Comprehensive display 7 6.3.5 Data Storage 8 6.3.6 One-button return 8 6.3.7 Automatic obstacle avoidance 8 6.3.8 Typical Failure Protection 8 6.3.9 Takeoff and Landing 8 6.3.10 Alarm 8 6.3.11 Motor Locking and Startup 9 6.3.12 Control mode switching 9 6.4 Flight performance 9 6.4.1 Maximum takeoff quality 9 6.4.2 Maximum working radius 9 6.4.3 Maximum flight altitude 9 6.4.4 Maximum flying speed 10 6.4.5 Maximum climb rate 10 6.4.6 Height retention performance 10 6.4.7 Speed Maintenance Performance 10 6.4.8 Life time 11 6.4.9 Fixed hover 11 6.4.10 Positioning navigation 12 6.4.11 Track accuracy 12 6.4.12 Wind resistance 12 6.5 Battery System 12 6.5.1 Charging time 12 6.5.2 Discharge capacity 13 6.5.3 Battery cycle life 13 6.5.4 Working condition cycle life 14 6.5.5 Overcharge 14 6.5.6 Over discharge 14 6.5.7 Short circuit 14 6.5.8 Low pressure 15 6.5.9 Drop 15 6.5.10 Temperature cycle 15 6.5.11 Squeeze 16 6.5.12 Heat abuse 16 6.5.13 Soaking 16 6.6 Navigation system 16 6.6.1 Static attitude accuracy 16 6.6.2 Static Positioning Accuracy 16 6.7 Data Link System 17 6.7.1 Remote telemetry distance 17 6.7.2 Information transmission distance 17 6.7.3 Transmitter RF output power 17 6.7.4 Receiver sensitivity 18 6.7.5 Transmitter spurious emission power 18 6.7.6 Transmitter adjacent channel leakage ratio 18 6.7.7 Carrier Center Frequency 18 6.7.8 Receiver adjacent channel selectivity 18 6.8 Environmental adaptability 19 6.8.1 High temperature 19 6.8.2 Low temperature 19 6.8.3 Rain 20 6.8.4 Damp heat 20 6.8.5 Vibration 20 6.8.6 Impact 20 6.9 Electromagnetic Compatibility 20 6.9.1 General 20 6.9.2 Launch test 21 6.9.3 Immunity 22 Appendix A (Normative Appendix) Remote Telemetry Distance Test Procedure 28

Foreword

This standard was drafted in accordance with the rules given in GB/T 1.1-2009. This standard is proposed and managed by the National Aircraft Standardization Technical Committee (SAC/TC435). This standard was drafted. China Aviation Integrated Technology Research Institute, Shenzhen Yidian Aviation Technology Co., Ltd., Shenzhen Dajiang Innovation Technology Company, Shenzhen Corbett Aviation Technology Co., Ltd., China Electronics Technology Standardization Research Institute, Shandong Luneng Intelligent Technology Co., Ltd., North Liaoning Zhuanglong UAV Technology Co., Ltd. The main drafters of this standard. Shu Zhenjie, Jia Bo, Hu Yingdong, Zeng Jia, Zhang Xianzhi, Yang Lan, Lu Zhihui, Luo Wei, Liu Wei, Quan Quan, Li Huanran, Wang Qiuyang, Zhang Chao, Lin Zhikun, Ma Zongfeng, He Zhikai, Che Jiaxing, Wu Anzhen, Huang Shan, Li Wanlong, Zhang Li, Chen Mingfei, Wang Bojia, Cao Guojie. Civil multi-rotor UAV system test method

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 missionprofile 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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