摘要
本文从飞行控制系统设计的角度出发,详细介绍了如何根据对某小型无人机特性的认识,进行小型化高性能飞行控制器的设计。硬件方面基于微控制模块586-Engine实现了飞行控制器的小型化设计。软件方面第一次实现了μC/OS-Ⅱ实时操作系统在SC520处理器上的移植,对飞行控制软件进行了模块化处理,并在二者基础上进行了合理的任务调度设计,实现了高性能设计。本系统已经通过半物理实时仿真,试验证明达到设计目标。
The paper describes how to design miniaturization high-powered flight control unit which is based on the research of UAV, in the view of flight control system design. About hardware design, we carry out miniaturization design of flight control unit based on 586-Engine. About software design, we transplant μC/OS-Ⅱto SC520 for the first time, and realize the module of flight control soft-ware. In this foundation, we make rational task scheduler, and achieve high-powered design. Now, this system had passed the half physical real-time emulation, the experimentation shows that the design is successful.
出处
《微计算机信息》
北大核心
2007年第19期16-18,共3页
Control & Automation
