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Delivery: <= 6 days. True-PDF full-copy in English will be manually translated and delivered via email. GB 42590-2023: Safety requirements for civil unmanned aircraft system Status: Valid
Basic dataStandard 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 table of contentsPreface 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 28forewordThis 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 systems1 ScopeThis 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 referencesThe 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: ......Tips & Frequently Asked Questions:Question 1: How long will the true-PDF of GB 42590-2023_English be delivered?Answer: Upon your order, we will start to translate GB 42590-2023_English as soon as possible, and keep you informed of the progress. 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