T/JSAMIA 2-2017 Agricultural Unmanned Aerial Vehicles (UAVs) Technical Requirements and Test Methods

Scope

Scope: This standard specifies the terms and definitions, abbreviations, technical requirements, and testing methods for agricultural drones (hereinafter referred to as "plant protection drones"). This standard applies to the design and manufacture of agricultural plant protection drones, their performance testing before launch, and their operational monitoring. Main technical content: 4.1 Main components of plant protection drones: airframe, power unit, avionics and electrical equipment, and mission equipment such as image acquisition devices, relay devices, electronic detection devices, delivery equipment, and rescue and auxiliary equipment. 4.2 Technical requirements 4.2.1 External dimensions Plant protection drones must clearly include information such as the drone's length and height. Multi-axis rotor plant protection drones must also include wheelbase and blade dimensions. Fixed-wing plant protection drones must include wing span dimensions. 4.2.2 External colors, markings, and safety signs 4.2.2.1 External colors The external body color of plant protection drones should be specified on the product label and packaging. If the purchaser has special requirements, they may be implemented according to the purchaser's specifications. 4.2.2.2 Markings Markings should indicate the product's model code, name, serial number, production date, manufacturer, and address. 4.2.2.3 Safety signs Safety signs should be installed at locations prone to human casualties in plant protection drones. Safety signs must comply with GB 10396-2006 and GB 10396. 4.2.3 Quality Plant protection drones should specify the following quality indicators in their design specifications: 4.2.3.1 Total drone weight The total drone weight includes mission weight, energy weight, and empty weight. Plant protection drones can be divided into maximum takeoff weight and empty takeoff weight based on their load capacity. 4.2.3.2 Mission weight The mission weight refe

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