介绍了基于PCI04的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,详细对惯性测量单元和电子罗盘进行了分析,系统具有设计精炼,可靠性高,可移植性强等特点
The article introduces the hardware Design of a UAV flight control system based on PC- 104, the design of system, selection of hardware are introduced. Especially, the analysis of inertial measure unit (IMU) and compass is introduced in detail. The design is noted for its simple structure, high reliability and opening.