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GB/T 38996-2020: General requirements for the flight control system of civil small and light fixed wing unmanned aircraft
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| Standard ID | Contents [version] | USD | STEP2 | [PDF] delivered in | Standard Title (Description) | Status | PDF |
| GB/T 38996-2020 | English | 339 |
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General requirements for the flight control system of civil small and light fixed wing unmanned aircraft
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GB/T 38996-2020
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PDF similar to GB/T 38996-2020
Standard similar to GB/T 38996-2020 GB/T 36258 GB/T 42856 GB/T 38997 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 | 18,154 | | 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)
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