GB/T 38997-2020 English PDFUS$339.00 · In stock
Delivery: <= 4 days. True-PDF full-copy in English will be manually translated and delivered via email. GB/T 38997-2020: General requirements for the flight control and navigation system of small and light multi-rotor unmanned aircraft Status: Valid
Basic dataStandard ID: GB/T 38997-2020 (GB/T38997-2020)Description (Translated English): General requirements for the flight control and navigation system of small and light multi-rotor unmanned aircraft Sector / Industry: National Standard (Recommended) Classification of Chinese Standard: V37 Classification of International Standard: 49.090 Word Count Estimation: 18,189 Date of Issue: 2020-07-21 Date of Implementation: 2021-02-01 Issuing agency(ies): State Administration for Market Regulation, China National Standardization Administration GB/T 38997-2020: General requirements for the flight control and navigation system of small and light multi-rotor unmanned aircraft---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. General requirements for the flight control and navigation system of small and light multi-rotor unmanned aircraft ICS 49.090 V37 National Standards of People's Republic of China Light and small multi-rotor drone flight General requirements for control and navigation systems 2020-07-21 released 2021-02-01 implementation State Administration for Market Regulation Issued 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 1 4 General requirements 2 4.1 System composition 2 4.2 Function, performance 2 4.3 Data record 6 4.4 Interface 6 4.5 Environmental adaptability 8 4.6 Electromagnetic compatibility 9 4.7 Reliability 9 4.8 Interchangeability 9 4.9 Use and maintenance 9 5 Proof test 10 5.1 Type test 10 5.2 Factory inspection 11 6 Identification, packaging, transportation and storage 11 6.1 General 11 6.2 Identification 11 6.3 Packaging 12 6.4 Transport 12 6.5 Storage 12ForewordThis standard was drafted in accordance with the rules given in GB/T 1.1-2009. This standard was proposed and managed by the National Aircraft Standardization Technical Committee (SAC/TC435). Drafting organizations of this standard. Shenzhen Dajiang Innovation Technology Co., Ltd., Yifei Intelligent Control (Tianjin) Technology Co., Ltd., China Aviation Technology Technology Research Institute, Shenzhen Corbet Aviation Technology Co., Ltd., Ewatt Technology Co., Ltd., Shenzhen United Aircraft Technology Co., Ltd., Beijing Dynamic Control Equipment Research Institute. The main drafters of this standard. Yang Yang, Cao Guojie, Lai Zhenzhou, Wu Chong, Hu Yingdong, Jia Jia, Shu Zhenjie, He Zhikai, Lu Zhihui, Che Jiaxing, Zhao Guocheng, Chen Jing, Ye Chuan, Liu Zhiqiang. Light and small multi-rotor drone flight General requirements for control and navigation systems1 ScopeThis 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 referencesThe 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 3.1 Terms and definitions The following terms and definitions defined in GB/T 35018 and GB/T 38152 apply to this document. 3.1.1 Fixed-point hover Under the condition of not receiving any external control instructions, the UAV keeps the relative position basically unchanged in the air. 3.2 Abbreviations The following abbreviations apply to this document. GNSS. Global Navigation Satellite System (GlobalNavigationSateliteSystem) IMU. Inertial Measurement Unit (Inertial Measurement Unit) SDK. Software Development Kit (SoftwareDevelopmentKit) ......Tips & Frequently Asked Questions:Question 1: How long will the true-PDF of GB/T 38997-2020_English be delivered?Answer: Upon your order, we will start to translate GB/T 38997-2020_English as soon as possible, and keep you informed of the progress. The lead time is typically 2 ~ 4 working days. The lengthier the document the longer the lead time.Question 2: Can I share the purchased PDF of GB/T 38997-2020_English with my colleagues?Answer: Yes. The purchased PDF of GB/T 38997-2020_English will be deemed to be sold to your employer/organization who actually pays for it, including your colleagues and your employer's intranet.Question 3: Does the price include tax/VAT?Answer: Yes. 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