GB/T 38996-2020
ActiveGeneral requirements for the flight control system of civil small and light fixed wing unmanned aircraft
民用轻小型固定翼无人机飞行控制系统通用要求
Application Summary AI generated
This standard specifies the general technical requirements, test methods, and acceptance criteria for flight control systems used in civil small and light fixed-wing unmanned aircraft. It is applied during the design, production, and quality inspection of such systems to ensure safe and reliable flight operations in civilian applications like aerial surveying, agriculture, and logistics. The standard covers functions including attitude control, navigation, and fault response for aircraft with a maximum takeoff mass under 150 kg.
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