摘要
介绍了一种新型的基于CAN总线的小型飞行器分布式伺服系统,描述了该系统的硬件结构,给出了系统CAN网络接口,并对系统中CAN网络通讯的实时性进行了分析。实验结果表明该系统运行良好,能够满足小型飞行器控制系统的要求。
The distributed servo system design for small aircraft was introduced; the hardware structure and the principle were described. The interface of CAN bus was given, and the real time ability of CAN bus was also analyzed. The experimental results indicate that the servo system works well and can meet the needs of flight control system.
出处
《弹箭与制导学报》
CSCD
北大核心
2008年第3期65-67,共3页
Journal of Projectiles,Rockets,Missiles and Guidance