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。
An organic whole and small scale of fault test and diagnosis system for UAV is realized and the result has satisfactory capability and value.
实现了无人机故障检测与诊断的一体化和小型化，具有良好的工程应用价值。
Design principles of the flight control and managing computer of a small reconnaissance UAV are presented.
论述一种小型无人侦察机的飞行控制与管理系统计算机的基本设计思想。
These features of UAV are especially suitable for small range of resource survey and disaster survey.
无人机这些特点尤其适用于小范围的资源调查和灾害调查。
A bus-structure flight control system using DSP as processor is designed, which aims at the demands of power, cost and integration from small Unmanned Aerial Vehicle(UAV).
针对小型无人机控制系统对功耗、成本、可集成性等的较高要求，设计了一种基于DSP芯片TMS320F2812的总线式飞行控制系统。
A bus-structure flight control system using DSP as processor is designed, which aims at the demands of power, cost and integration from small Unmanned Aerial Vehicle(UAV).
针对小型无人机控制系统对功耗、成本、可集成性等的较高要求，设计了一种基于DSP芯片TMS320F2812的总线式飞行控制系统。
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