The design of a unitary fuel tank for small UAV is presented.
介绍小型无人机整体油箱的研制。
Bases on the aircraft structure fatigue life theory, consider the characteristics of small UAV, the model of fatigue life prediction for small UVA structure is established.
在飞机结构寿命理论的基础上，结合小型无人机机体结构特点，建立了小型无人机机体寿命分析方法。
The whole system takes on characteristics of various of functions, small volume, little weight, low consumption and high integration, and it suits for applying to small UAV.
本系统具有功能全、体积小、重量轻、功耗低、集成度高等特点，非常适合应用于小型无人机。
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