GB/T 43369-2023Interface requirements of electro-optical mission payload equipment of civil large and medium unmanned aircraft (English PDF)
民用大中型无人机光电任务载荷设备接口要求
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Issued by
SAMR; SAC
Level / Type
National · Recommended
Issue date
November 27, 2023
Implementation date
March 1, 2024
Scope
GB/T 43369-2023 is the English-translated version of 民用大中型无人机光电任务载荷设备接口要求.
GB/T 43369-2023 fixes the interface between the electro-optical mission payload equipment of large and medium civil unmanned aircraft and the aircraft itself.
Clause 1 covers the general and detailed requirements for both the mechanical and the electrical interface, and the contents list adds function, equipment class, reliability, security, maintainability, electromagnetic compatibility and environmental adaptability, plus informative annexes giving a mechanical interface guide and an electrical interface guide.
Clause 1 states that it applies to electro-optical mission payload equipment with a rotation diameter of 120 mm to 500 mm on civil unmanned aircraft whose maximum take-off weight is not less than 150 kg, other payload equipment mounted on unmanned aircraft being able to use it for reference.
It quotes GB/T 30203, GB/T 35018 and GB/T 38152. Issued on 27 November 2023, it has applied since 1 March 2024.
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Document preview — GB/T 43369-2023
National Standard of the People's Republic of China
- ICS
- 49.020
- Classification
- V 20
Issued by: State Administration for Market Regulation; Standardization Administration of the PRC
Contents
- Preface
- 1 Scope
- 2 Normative references
- 3 Terms and Definitions
- 4 Abbreviations
- 5 General requirements
- 5.1 Function
- 5.2 Equipment class
- 5.3 Reliability
- 5.4 Security
- 5.5 Guarantee
- 5.6 Maintainability
- 5.7 Electromagnetic compatibility
- 5.8 Environmental adaptability
- 6 Detailed requirements
- 6.1 Mechanical interface
- 6.2 Electrical interface
- Appendix A (informative) Optoelectronic mission payload equipment mechanical interface guide
- Appendix B (informative) Optoelectronic mission payload equipment electrical interface guide
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.
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 electro-optical mission payload equipment
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 Rotation diameter
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)
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This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — 15 pages — is available in the English PDF.
Referenced standards
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Related Standards
GB/T 30203-2013 — Characteristics of aircraft electrical system
GB/T 35018-2018 — Classification and grading for civil unmanned aircraft system
GB/T 38152-2019 — Terminology for unmanned aircraft system
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GB/T 43369-2023
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