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Basic data
| Standard ID | GA/T 1411.1-2017 (GA/T1411.1-2017) |
| Description (Translated English) | Police unmanned aircraft systems��Part 1: General technical requirements |
| Sector / Industry | Public Security (Police) Industry Standard (Recommended) |
| Classification of Chinese Standard | A94 |
| Classification of International Standard | 49.020 |
| Word Count Estimation | 14,193 |
| Date of Issue | 2017-08-28 |
| Date of Implementation | 2017-08-28 |
| Issuing agency(ies) | Ministry of Public Security |
GA/T 1411.1-2017: Police unmanned aircraft systems—Part 1: General technical requirements
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Police unmanned aircraft systems-Part 1. General technical requirements
ICS 49.020
A94
People's Republic of China public safety industry standards
Police unmanned aircraft system
Part 1. General technical requirements
Part 1.Generaltechnicalrequirements
2017-08-28 Posted
2017-08-28 Implementation
Ministry of Public Security of People's Republic of China released
Foreword
GA/T 1411 "Police Unmanned Aerial Vehicle System" is divided into the following sections.
--- Part 1. General technical requirements;
--- Part 2. Unmanned helicopter system;
--- Part 3. Multi-rotor unmanned aircraft systems;
--- Part 4. Fixed-wing unmanned aircraft systems;
This part of GA/T 1411 Part 1.
This section drafted in accordance with GB/T 1.1-2009 given rules.
This section proposed by the Ministry of Public Security Equipment Finance Bureau.
This part of the National Police Standardization Technical Committee (SAC/TC561) centralized.
This part of the drafting unit. Ministry of Public Security Equipment Finance Bureau, Ministry of Public Security Police Aviation Management Office, the Ministry of Public Security Institute, Shenzhen, an electric
Air Technology Co., Ltd., Ministry of Public Security Special Police Equipment Quality Supervision and Inspection Center, Beijing CATIC Technology Co., Ltd., China Aerospace Science and Technology Set
Ninth Academy of Corps unmanned aerial systems Engineering Research Institute, Hefei good news Technology Co., Ltd., Eagle International Aviation Technology Co., Ltd., Shenzhen Branch
Weitai Industrial Development Co., Ltd., Yi Watts Technology Co., Ltd., Shenzhen Zhongyi Special Equipment Manufacturing Co., Ltd.
The main drafters of this section. Shi Guangming, Hu Jianting, Sun Fei, Zhang Xianzhi, Lu Xiaoke, satisfied, Zhang Guoyong, Zhang Song, Sun Zhijian, Li Jiansheng,
Zhao Guocheng, Xu Xu.
This section was first released in August.2017.
Police unmanned aircraft system
Part 1. General technical requirements
1 Scope
This part of GA/T 1411 specifies the terms and definitions, classifications and designations of the general technical requirements for a police unmanned aircraft system,
Technical requirements, packaging, transportation and storage.
This section applies to the police unmanned aircraft system.
2 Normative references
The following documents for the application of this document is essential. For dated references, only the dated version applies to this article
Pieces. For undated references, the latest edition (including all amendments) applies to this document.
Safety precautions alarm equipment safety requirements and test methods GB 16796-2009
Electromagnetic compatibility (EMC) test and measurement techniques Electrostatic discharge (IMD) immunity test
GB/T 17626.3-2016 Electromagnetic compatibility testing and measurement techniques RF electromagnetic field radiation immunity test
General Requirements for UAV Measurement and Control System
3 Terms and definitions
The following terms and definitions apply to this document.
3.1
Police unmanned aircraft policeunmannedaircraft
Aircraft that are equipped by the public security organ and are suitable for the execution of police duties, that are not controlled by the pilot onboard the aircraft, including autonomous aircraft and remote control
Driving aircraft, excluding aeronautical models, unmanned free balloons, tethered balloons, and aircraft for special policing needs.
3.2
Police unmanned aircraft system policeunmannedaircraftsystem
A system of police unmanned aircraft and its associated control stations (stations), required command and control links, etc.
3.3
Fixed-wing unmanned aircraft fixed-wingunmannedaircraft
Unmanned aerial vehicles powered by fixed wings.
3.4
Unmanned helicopter unmanned helicopter
Unmanned aerial vehicles with one or two rotors, capable of vertical takeoff and landing and free hovering.
3.5
Multi-rotor unmanned aircraft multi-axisunmannedaircraft
Unmanned aerial vehicles with three or more rotors, capable of vertical take-off and landing, free hovering.
3.6
Control station controlstation
For mission planning, link control, flight control, load control, track display, parameter display, image display and load information display
...
