GB/T 44166-2024 English PDF

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GB/T 44166-2024: Flight test requirements for autonomous capability of civil large and medium-sized fixed-wing unmanned aircraft system
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Basic data

Standard ID: GB/T 44166-2024 (GB/T44166-2024)
Description (Translated English): Flight test requirements for autonomous capability of civil large and medium-sized fixed-wing unmanned aircraft system
Sector / Industry: National Standard (Recommended)
Classification of Chinese Standard: V35
Classification of International Standard: 49.020
Word Count Estimation: 14,172
Date of Issue: 2024-06-29
Date of Implementation: 2025-01-01
Issuing agency(ies): State Administration for Market Regulation, China National Standardization Administration

GB/T 44166-2024: Flight test requirements for autonomous capability of civil large and medium-sized fixed-wing 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.
Flight test requirements for autonomous capability of civil large and medium-sized fixed-wing unmanned aircraft system Autonomous capabilities of large and medium-sized civil fixed-wing UAV systems Flight test requirements Flight test requirements for autonomous capability of civil large and medium-sized fixed-wing unmanned aircraft system ICS 49.020 CCS V 35 National Standards of People's Republic of China Released on 2024-06-29 2025-01-01 Implementation State Administration for Market Regulation The National Standardization Administration issued

Table of Contents

Preface ... 1 Scope ... 2 Normative referenced documents ... 3 Terms and Definitions ... 4 General requirements ... 4.1 Flight Test Conditions ... Drafting is required. Please note that some of the contents of this document may involve patents. The issuing organization of this document does not assume the responsibility for identifying patents. This document is proposed and coordinated by the National Technical Committee for Aircraft Standardization (SAC/TC 435). This document was drafted by. China Flight Test Establishment, China Aviation Technology Research Institute, AVIC Guizhou Aircraft Co., Ltd., Aisen UAV test and testing Jingbian Co., Ltd., Beijing Institute of Technology, Xi'an Lingkong Electronic Technology Co., Ltd. The main drafters of this document are. Zhang Peitian, Wu Xinlong, Shu Zhenjie, He Zhengyan, Tang Jian, Wang Feng, Hu Yingdong, Qi Shengjun, An Ran, Pan Jihui, Zhong Hai, Xi Liangliang, Wang Yalong, Li Jian, Dai Liugang, Wang Jiuyuan, Han Chenglin, Zhang Zejing, Liao Xintao, Liu Guanyong, Sun Youbin and Wang Yanping. Autonomous capabilities of large and medium-sized civil fixed-wing UAV systems Flight test requirements

1 Scope

This document specifies the general flight test procedures for autonomous capability of civil large and medium-sized fixed-wing unmanned aerial vehicle systems (hereinafter referred to as "unmanned aerial vehicle systems"). Requirements, flight capabilities, operational risk factor identification and response capabilities, manual intervention capabilities and flight test report requirements. This document is applicable to the autonomous capability flight test of large and medium-sized civil fixed-wing UAV systems and other types of UAV system autonomous capability flight The test is carried out according to the reference.

2 Normative references

The contents of the following documents constitute the essential clauses of this document through normative references in this document. For referenced documents without a date, only the version corresponding to that date applies to this document; for referenced documents without a date, the latest version (including all amendments) applies. in this document. GB/T 35018 Classification and classification of civil unmanned aerial vehicle systems GB/T 38152 Terminology of Unmanned Aircraft Systems

3 Terms and definitions

The terms and definitions defined in GB/T 35018, GB/T 38152 and the following apply to this document. 3.1 Autonomous capability The ability of an unmanned aerial vehicle system to fly in autonomous or automatic mode within its designed operating range and to identify and respond to operational risk factors. Note 1.Autonomous mode means that the UAV system operator does not intervene in the flight, and the decision is based on the judgment of the UAV system. Note 2.The automatic mode is executed according to the pre-set program. Important decisions are based on human judgment and require the UAV system operator to send instructions. 3.2 unmanned aircraft system pilot Operators involved in the flight of an unmanned aerial vehicle system. 3.3 Operational risk identification and response Identify variables that could reduce the level of operational safety and respond appropriately.

4 General requirements

4.1 Flight test conditions The test site conditions (altitude, runway, etc.) and environmental conditions (such as atmospheric temperature, atmospheric pressure, atmospheric humidity, wind speed, wind direction, visibility, electromagnetic environment, etc.) should comply with the technical requirements of the UAV system. The operational risk identification and response capability test flight subjects should first perform ground tests, and then conduct relevant tests after evaluating the validity of the ground test results. Applicable flight tests. ......

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