【摘要】 介绍了基于PC104小型无人机飞行控制系统的硬件实现,给出了系统整体方案的设计和具体的硬件选型,详细地分析了惯性测量单元、电子罗盘、转速传感器、声纳。同时在设计中绝大多数元器件采用最小型号的贴片封装,使该硬件平台具有设计精炼、可靠性高、可移植性强等特点,系统在飞行器多次试飞后,证明是实用的。更多还原

【Abstract】 The hardware design of a UAV flight control system based on PC-104 is introduced,the design of system,selection of hardware are introduced.Especially,the analysis of inertial measure unit(IMU),compass,RPM sensor and sonar is introduced in detail.Because of the minimum package of the most elements,the hardware platform is noted for its simple structure,high reliability and opening.The experimental result show that the system is applied.更多还原