摘要
主要介绍了基于交流伺服电机的飞行器模型姿态角控制系统的硬件组成和软件功能,控制系统结合了交流伺服电机、伺服单元、工业控制计算机(工控机)和可编程逻辑控制器PLC的优点,当模型名义角度在-4°～12°之间时,角度控制精度都在±1'以内,接近国军标先进水平。
The hardware and software features of aircraft model attitude control systems based on AC servo motor are introduced.The control system combines the advantages of combining with AC servo motors,servo units,industrial computer（IPC）,PLC.When the given angle of the control model is between-4°~12°,the accuracy of the control system is smaller than ±1′,which is close to the advanced level of the GJB in China.
出处
《测控技术》
CSCD
北大核心
2011年第7期46-48,共3页
Measurement & Control Technology
基金
西北工业大学科技创新基金资助项目(2010KJ0101)
关键词
伺服电机
模型姿态角
控制系统
servo motor
aircraft model attitude
control system
