摘要
在实时操作系统μC/OS-Ⅱ的基础上,设计了空空导弹舵机控制系统。任务调度算法RMS和仿真试验分别从理论和试验角度验证了该系统的可行性。该系统在保证控制精度和实时性的基础上,为开发人员提供方便的接口。
An airborne missile rudder controlling system is designed based on the real-time operation system μC/OS-Ⅱ.It is proved by task scheduling algorithm RMS and the experiment results.The precise controlling and real-time response are achieved in the system,while the convenient interface for the programmer is another key point.
出处
《航空计算技术》
2009年第5期122-124,共3页
Aeronautical Computing Technique
