小型四旋翼飞行器由于具有体积小、结构简单、设计简便,能够在多种复杂环境下开展作业,因而深受军工以及民用领域的青睐。然而,小型四旋翼飞行器具备独特的动力学特征,需要在试验平台上进行仿真测试。所以,小型四旋翼飞行器试验平台的设计工作成为当前学术领域新兴研究课题之一。而本文将对其试验平台设计展开深入分析,总结设计经验。 Small four-rotor aircraft due to its small size, simple structure, easy to design, can operate in a variety of complex environments, and therefore by the military and civilian areas of all ages. However, the small quadrotors have unique kinetic characteristics that require simulation testing on a test rig. Therefore, the design of a small quadrotor pilot platform has become one of the emerging research topics in current academic fields. This article will conduct in-depth analysis of its experimental platform design, summed up the design experience.