Home Cart Quotation Policy About-Us
www.ChineseStandard.net
Database: 221581 (27 Mar 2026)
SEARCH
Path: Home > GB/T > Page31 > GB/T 38996-2020

GB/T 38996-2020 PDF English

Price & Delivery

US$339.00 · In stock · Download in 9 seconds
GB/T 38996-2020: General requirements for the flight control system of civil small and light fixed wing unmanned aircraft
Delivery: 9 seconds. True-PDF full-copy in English & invoice will be downloaded + auto-delivered via email. See step-by-step procedure
Status: Valid
Std IDVersionUSDBuyDeliver [PDF] inTitle (Description)
GB/T 38996-2020English339 Add to Cart 4 days [Need to translate] General requirements for the flight control system of civil small and light fixed wing unmanned aircraft

Click to Preview a similar PDF

Basic data

Standard ID GB/T 38996-2020 (GB/T38996-2020)
Description (Translated English) General requirements for the flight control system of civil small and light fixed wing unmanned aircraft
Sector / Industry National Standard (Recommended)
Classification of Chinese Standard V37
Classification of International Standard 49.090
Word Count Estimation 18,153
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 38996-2020: General requirements for the flight control system of civil small and light fixed wing 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 system of civil small and light fixed wing unmanned aircraft ICS 49.090 V37 National Standards of People's Republic of China Civil light and small fixed-wing UAV flight control system common enquiries 2020-07-21 released 2021-02-01 implementation State Administration for Market Regulation Issued by the National Standardization Management Committee

Table of contents

Preface 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 Function 2 4.2 Performance 6 4.3 Components 8 4.4 Interface 9 4.5 Software 11 4.6 Security 11 4.7 Reliability 11 4.8 Maintainability 11 4.9 Environmental adaptability 11 4.10 Electromagnetic compatibility 11 4.11 Use and maintenance 11 5 Proof test 12 5.1 Test type 12 5.2 Type test 13 5.3 Factory inspection 13 6 Identification, packaging, transportation and storage 13 6.1 Identification 13 6.2 Packaging 14 6.3 Transportation and storage 14

Foreword

This 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. China Aviation Industry Corporation Xi’an Flight Automatic Control Research Institute, Guangdong Taiyi High-tech Development Co., Ltd. Division, Northwestern Polytechnical University, China Aviation Technology Research Institute, Ewatt Technology Co., Ltd., Xi'an Aisheng Technology Group Company, Beijing Space Aircraft overall design department. The main drafters of this standard. Xiang Xin, Hu Yingdong, Wang Rui, Huang Shan, Yang Guoqiang, Zhang Xiaolin, Zhao Guocheng, Zhang Ning, Pan Jihui, Shu Zhenjie, Cao Guojie, Xiao Ying, Liu Jian, Yu Qingsong, Ye Chuan. Civil light and small fixed-wing UAV flight control system common enquiries

1 Scope

This standard specifies general requirements, verification tests, and verification tests for civil light and small fixed-wing UAVs (hereinafter referred to as "UAVs") flight control systems Identification, packaging, transportation and storage. This standard applies to civil light and small fixed-wing UAV flight control systems with a maximum take-off weight between 0.25kg and 150kg. The design and verification of its components can be implemented by reference to other UAV flight control systems.

2 Normative references

The 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 8566 Information Technology Software Life Cycle Process GB/T 9254-2008 Information Technology Equipment Radio Disturbance Limits and Measurement Methods GB/T 14394 Computer software reliability and maintainability management 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 (all parts) Environmental test methods for civil light and small UAV systems 3 Terms, definitions and abbreviations 3.1 Terms and definitions The terms and definitions defined in GB/T 35018 and GB/T 38152 apply to this document. 3.2 Abbreviations The following abbreviations apply to this document. ADS-B. Automatic dependent surveillance (AutomaticDependentSurveilance-Broadcast) CAN. Controller Area Network Bus (ControlerAreaNetwork) GNSS. Global Navigation Satellite System (GlobalNavigationSateliteSystem) IMU. Inertial Measurement Unit (Inertial Measurement Unit) UART. Universal Asynchronous Receiver/Transmitter (UniversalAsynchronousReceiver/T ransmitter) USB. Universal Serial Bus (UniversalSerialBus)
...

Refund Policy Privacy Policy Terms of Service