轻型无人机的设计与开发

Design and Development of Light UAV

本研究设计开发了一款能够自主巡航并巡检的轻型固定翼轻木无人机,其具备陆地滑跑和水面滑行起降的能力。首先进行概念设计,明确功能目标和性能目标;其次进行初步设计,确定无人机的总体布局和结构参数;再次进行方案设计,包括气动分析和操稳特性分析;之后进行详细设计,包括二维图纸的绘制和三维模型的装配;最后进行零部件的加工和样机装调,并进行试飞和功能验证。试验结果表明,该流程能够高效地完成一款轻型固定翼无人机的设计开发工作,并实现其相关功能。

A light fixed-wing UAV capable of autonomous cruise and inspection is designed and produced,it has the ability to land and take off on land and water.First, oncept design is carried out to clarify functional and performance goals.Secondly,preliminary design is carried out to determine the overall layout and structural parameters of the UAV.Thirdly,schematic design is carried out, including aerodynamic analysis and handling stability analysis.Fourth,detailed design is carried out,including 2D Drawing,3D model assembly.Finally,parts processing and prototype assembly is carried out,as well as test flight and functional verification.The results show that the process can efficiently complete the design and development of a light fixed wing UAV and realize related functions.