基于ARM的小型无人机飞行控制器设计  

Hardware Design of Flight Control System for UAV Based on ARM

作　　者：李硕[1] 李小民[1] 

机构地区：[1]军械工程学院光学与电子工程系,河北石家庄050003

出　　处：《微计算机信息》2007年第29期133-135,共3页Control & Automation

基　　金：国家自然科学基金资助项目(F010103)

摘　　要：飞行控制器是无人机飞行控制系统的核心。采用ARM做为微处理器,结合MEMS传感器设计小型无人机飞行控制器。分析系统的功能和结构,并分为微处理器单元、导航传感器单元和气压传感器单元分别进行详细的功能和结构介绍。此设计符合飞行控制器的性能好、可靠性高、综合化能力强的发展趋势,具有广泛的应用前景。The flight control equipment is a kernel of unmanned aircraft flight system. The flight control equipment is based on MEMS sensors and ARM processor which select as its core. The system function and structure are analyzed, The ARM processor part ,navigation sensors part and air pressure data sensors part are the three part which function and structure are particular introduced. The flight control equipment meet the trend of high performance ,reliability and integration, and With the most potential for market growth of small UAVs.

关 键 词：无人机 飞行控制 ARM处理器 传感器 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计]