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GB 42590-2023 English PDF

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GB 42590-2023: Safety requirements for civil unmanned aircraft system
Status: Valid

Standard ID	Contents [version]	USD	STEP2	[PDF] delivered in	Standard Title (Description)	Status	PDF
GB 42590-2023	English	799	Add to Cart	6 days [Need to translate]	Safety requirements for civil unmanned aircraft system	Valid	GB 42590-2023

PDF similar to GB 42590-2023

Standard similar to GB 42590-2023

GB/T 36258 GB/T 44167 GB/T 44166

Basic data

Standard ID	GB 42590-2023 (GB42590-2023)
Description (Translated English)	Safety requirements for civil unmanned aircraft system
Sector / Industry	National Standard
Classification of Chinese Standard	V35
Classification of International Standard	49.020
Word Count Estimation	39,379
Date of Issue	2023-05-23
Date of Implementation	2024-06-01
Issuing agency(ies)	State Administration for Market Regulation, China National Standardization Administration

GB 42590-2023: Safety requirements for civil 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.
ICS 49:020 CCSV35 National Standards of People's Republic of China Safety requirements for civil unmanned aircraft systems Released on 2023-05-23 2024-06-01 Implementation State Administration for Market Regulation Released by the National Standardization Management Committee

Preface III 1 Scope 1 2 Normative references 1 3 Terms, Definitions and Abbreviations 1 3:1 Terms and Definitions 1 3:2 Abbreviations 2 4 Security requirements 2 4:1 Geo-fence 2 4:2 Remote identification 2 4:3 Emergency treatment 2 4:4 Structural Strength 2 4:5 Body structure 3 4:6 The whole machine falls 3 4:7 Power energy system 4 4:8 Controllability 6 4:9 Error proofing 6 4:10 Sense and avoid 6 4:11 Data link protection 6 4:12 Electromagnetic Compatibility 6 4:13 Wind resistance 6 4:14 Noise 7 4:15 Lighting 7 4:16 Identification 7 4:17 User Manual 8 5 Test method 8 5:1 Geo-fence 8 5:2 Remote identification 9 5:3 Emergency treatment 9 5:4 Structural strength 10 5:5 Body structure 10 5:6 The whole machine falls 10 5:7 Power energy system 11 5:8 Controllability 16 5:9 Anti-error safety test 19 5:10 Sense and avoid 20 5:11 Data link protection 20 5:12 Electromagnetic Compatibility 21 5:13 Wind resistance 21 5:14 Noise test 21 5:15 Lighting 25 5:16 Identification 26 5:17 User Manual 26 6 Implementation of Standards 26 Appendix A (Normative) Remote Identification 27 A:1 Remote identification requirements 27 A:2 Test method 28

foreword

This document is in accordance with the provisions of GB/T 1:1-2020 "Guidelines for Standardization Work Part 1: Structure and Drafting Rules for Standardization Documents" drafting: Please note that some contents of this document may refer to patents: The issuing agency of this document assumes no responsibility for identifying patents: This document is proposed and managed by the Ministry of Industry and Information Technology of the People's Republic of China: Safety requirements for civil unmanned aircraft systems

1 Scope

This document specifies the safety requirements for civil unmanned aircraft system products (hereinafter referred to as "unmanned aircraft"), and describes the relevant Appropriate test method: This document applies to micro unmanned aircraft, light unmanned aircraft and small unmanned aircraft development, production, delivery and use:

2 Normative references

The contents of the following documents constitute the essential provisions of this document through normative references in the text: Among them, dated references For documents, only the version corresponding to the date is applicable to this document; for undated reference documents, the latest version (including all amendments) is applicable to this document: GB/T 3222:2-2022 Description, Measurement and Evaluation of Acoustic Environmental Noise Part 2: Determination of Sound Pressure Level GB/T 17626:2-2018 Electromagnetic Compatibility Test and Measurement Technology Electrostatic Discharge Immunity Test GB/T 20441:4-2006 Measurement microphones Part 4: Specifications for working standard microphones GB/T 35018-2018 Classification and classification of civil unmanned aircraft systems GB/T 38152-2019 Terminology for unmanned aircraft systems GB/T 38909-2020 Electromagnetic Compatibility Requirements and Test Methods for Civil Light and Small UAV Systems GB/T 38930-2020 Requirements and test methods for wind resistance of civil light and small UAV systems GB/T 41300-2022 Civil UAV unique product identification code 3 Terms, Definitions and Abbreviations 3:1 Terms and Definitions GB/T 35018-2018, GB/T 38152-2019 and the following terms and definitions apply to this document: 3:1:1 unmanned aircraft unmannedaircraft; UA An aircraft with a self-contained power system without an onboard pilot: Note: Divided into micro, light, small, medium and large: 3:1:2 The weight of the empty aircraft is less than 0:25kg, the maximum flight height does not exceed 50m, the maximum level flight speed does not exceed 40km/h, and the radio transmission device It is an unmanned aircraft that meets the technical requirements of micro-power short-distance and can be controlled manually at any time during the whole process: 3:1:3 The weight of the empty aircraft does not exceed 4kg, the maximum take-off weight does not exceed 7kg, and the maximum level flight speed does not exceed 100km/h It is an unmanned aircraft that can maintain the airspace required by management and be reliably monitored, and can be manually controlled at any time throughout the process:

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