基于CAN总线的小型无人机飞控系统设计  

Design of Flight Control System Based on CAN-BUS for Small UAV

作　　者：刘银春[1] 何清华[2] 贺继林[2] 

机构地区：[1]中南大学机电工程学院,湖南长沙410083 [2]中南大学

出　　处：《微计算机信息》2008年第28期23-25,共3页Control & Automation

摘　　要：高性能和小型化的发展趋势,本文采用CAN总线技术,以PC/104模块板为核心,完成了新型无人机飞行控制器的硬件设计,详细给出了系统整体方案的分析设计和具体的硬件选型及接口设计。对设计中的关键技术进行了研究,系统具有设计精炼,可靠性高,开放性等特点。In order to follow the development trend of high performance and small size of flight control system for UAV, this paper adopted CAN-Bus technology, completed a new design of autopilot for small UAV based the board of PC104, and presented the whole system analysis, selection of hardware, design Of communication interface in detail.The key techniques related to hardware design are discussed.The design is noted for its simple structure, high reliability and opening.

关 键 词：CAN总线 飞控系统 无人机 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计]