摘要
以AT91M55800A微控器为核心设计并实现了基于ARM的新型无人机飞行控制器,详细给出了无人机飞行控制系统的设计原理和控制策略,介绍了基于μC/OS-Ⅱ实时操作系统的飞行控制软件的功能模块和任务划分方法,着重说明了各个任务之间的任务调度策略;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。
The design theory and control policy of digital flight control system are described in detail based on ARM for UAV. And the function module of real time control software is also introduced. The key techniques related to design are discussed. The design is noted for its simple structure, high reliability, system-opening etc.
出处
《计算机测量与控制》
CSCD
2005年第10期1063-1065,1068,共4页
Computer Measurement &Control
