伺服系统
Minimum weight and volume are almost overriding requirements for any missile servo. 对于任何一种导弹的伺服系统来说，使它的重量为最轻和体积为最小，几乎是最主要的要求了。
Experimental results show the superiority of the proposed multimicroprocessor-based AC induction servo system. 实验解果可显示此一交流感应伺服系统良好之稳态与暂态响应。
