Path:
Home >
GB/T >
Page30 > GB/T 43369-2023
Price & Delivery
US$269.00 · In stock · Download in 9 secondsGB/T 43369-2023: Interface requirements of electro-optical mission payload equipment of civil large and medium unmanned aircraft
Delivery: 9 seconds. True-PDF full-copy in English & invoice will be downloaded + auto-delivered via email. See
step-by-step procedureStatus: Valid
| Std ID | Version | USD | Buy | Deliver [PDF] in | Title (Description) |
| GB/T 43369-2023 | English | 269 |
Add to Cart
|
3 days [Need to translate]
|
Interface requirements of electro-optical mission payload equipment of civil large and medium unmanned aircraft
|
Click to Preview a similar PDF
Basic data
| Standard ID | GB/T 43369-2023 (GB/T43369-2023) |
| Description (Translated English) | Interface requirements of electro-optical mission payload equipment of civil large and medium unmanned aircraft |
| Sector / Industry | National Standard (Recommended) |
| Classification of Chinese Standard | V20 |
| Classification of International Standard | 49.020 |
| Word Count Estimation | 13,152 |
| Date of Issue | 2023-11-27 |
| Date of Implementation | 2024-03-01 |
| Issuing agency(ies) | State Administration for Market Regulation, China National Standardization Administration |
GB/T 43369-2023: Interface requirements of electro-optical mission payload equipment of civil large and medium 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.
ICS 49:020
CCSV20
National Standards of People's Republic of China
Civilian large and medium-sized UAV photoelectric missions
Payload device interface requirements
Published on 2023-11-27
2024-03-01 Implementation
State Administration for Market Regulation
Released by the National Standardization Administration Committee
Table of contents
Preface III
1 Scope 1
2 Normative references 1
3 Terms and Definitions 1
4 Abbreviations 1
5 General requirements 2
5:1 Function 2
5:2 Equipment class 2
5:3 Reliability 2
5:4 Security 2
5:5 Guarantee 2
5:6 Maintainability 2
5:7 Electromagnetic compatibility 2
5:8 Environmental adaptability 2
6 Detailed requirements 3
6:1 Mechanical interface 3
6:2 Electrical interface 3
Appendix A (informative) Optoelectronic mission payload equipment mechanical interface guide 5
Appendix B (informative) Optoelectronic mission payload equipment electrical interface guide 7
Foreword
This document complies with the provisions of GB/T 1:1-2020 "Standardization Work Guidelines Part 1: Structure and Drafting Rules of Standardization Documents"
Drafting:
Please note that some contents of this document may involve patents, and the issuing organization of this document does not assume the responsibility for identifying patents:
This document is proposed and coordinated by the National Aircraft Standardization Technical Committee (SAC/TC435):
This document was drafted by: Aviation Industry Corporation of China Luoyang Electro-Optical Equipment Research Institute, China Aviation Comprehensive Technology Research Institute, Beijing Aviation Industry Corporation
University of Aeronautics and Astronautics, Xi'an Aisheng Technology Group Co:, Ltd:, Beijing Space Vehicle Overall Design Department, Nanjing University of Aeronautics and Astronautics:
The main drafters of this document: Lu Gaojie, Shu Zhenjie, Lu Changyi, Tang Tang, Qi Liqiang, Zhang Zejing, Wang Zengguang, Zeng Qingyong, Lai Jizhou, Liu He,
Lu Pin, Liu Jian, Che Jiaxing, Wang Jiuyuan, Hu Yingdong, Sun Hengyi, Du Juan:
Optoelectronic missions of large and medium-sized civilian UAVs
Payload device interface requirements
1 Scope
This document specifies the general requirements for the mechanical interface and electrical interface between the optoelectronic mission load equipment of large and medium-sized civilian UAVs and the UAV:
and detailed requirements:
This document is applicable to civil UAVs with a maximum takeoff weight of not less than 150kg and a rotation diameter of 120mm~500mm:
Optoelectronic mission load equipment, other optoelectronic mission load equipment mounted on UAVs can be used as reference:
2 Normative reference documents
The contents of the following documents constitute essential provisions of this document through normative references in the text: Among them, the dated quotations
For undated referenced documents, only the version corresponding to that date applies to this document; for undated referenced documents, the latest version (including all amendments) applies to
this document:
GB/T 30203 Aircraft electrical system characteristics
GB/T 35018 Classification and classification of civil unmanned aircraft systems
GB/T 38152 Unmanned aircraft system terminology
3 Terms and definitions
The following terms and definitions as defined in GB/T 35018 and GB/T 38152 apply to this document:
3:1
The UAV is equipped with any sensor that can adapt to the working environment and is integrated with one or more photoelectric sensors such as ultraviolet, infrared, visible light and laser:
The service load has the ability to use the difference between the target and the background reflected or radiated light waves to achieve imaging observation of the target, and obtain the video image and target of the target:
Devices with information functions such as marking location:
3:2
rotationdiameter rotationdiameter
The diameter of the largest circle on the outer edge of the main frame of the optoelectronic mission payload equipment is used to characterize the maximum space inside the equipment:
4 Abbreviations
The following abbreviations apply to this document:
USB: Universal Serial Bus (UniversalSerialBus)
...
