测控技术2011，Vol.30Issue(7)：46-48,3.
基于伺服电机的飞行器模型姿态角控制系统
Aircraft Model Attitude Control System Based on Servo Motor
摘要
Abstract
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 u-nits, 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.关键词
伺服电机/模型姿态角/控制系统Key words
servo motor/ aircraft model attitude/ control system分类
航空航天引用本文复制引用
惠增宏,柳雯..基于伺服电机的飞行器模型姿态角控制系统[J].测控技术,2011,30(7):46-48,3.基金项目
西北工业大学科技创新基金资助项目(2010KJ0101) （2010KJ0101）
