摘要
介绍了一种导弹舵机控制实验系统。对其软、硬件结构进行了设计,将本系统模块化为图形用户界面模块、控制律模块和应用程序模块,主要针对控制律模块进行了详细设计。使同一系统可加载三环、PID、用户自定义等3种控制类型、11种控制方式的控制律。尤其是自定义控制的加载,有益地改善了用户的设计效率。同时,嵌入式设计的引入,有效地增强了系统的实时性。
The experiment system used to control missile rudderh is described. The structure of software and hardware is designed. The system is modularized into GUI, control law and application program module, and control law module is designed particularly. 3-loop control, PID control and DIY control which sum to 3 types or 11 modes of control can be loaded to the system. Especially using the load of DIY control law, the design efficiency is improved greatly. Meanwhile, the character of real time is enhanced due to introducing the idea of embedded Linux.
出处
《测控技术》
CSCD
2006年第12期22-25,共4页
Measurement & Control Technology
基金
国家航天基金资助项目(N4CH008)
航空基础科学基金资助项目(04I53067)
