摘要
舵机是导弹飞行控制系统的执行机构,导弹的各种姿态运动都是靠舵机带动舵面偏转来实现的。文章在详细介绍舵机仿真器硬件设计基础上,完成了系统软件设计,对伺服系统进行了仿真,分析了系统的性能。
Missile rudders are executive bodies of missile flight control system. All kinds of attitude motion of missile are depended on the actuator driver fins of rudder. The software designs of the electrical servo system were completed after the hardware designs were presented in details. Then simulation and analysis of the servo system were carried out.
出处
《海军航空工程学院学报》
2008年第2期132-134,共3页
Journal of Naval Aeronautical and Astronautical University
关键词
舵机
伺服系统
控制器设计
仿真
rudder
servo system
designs of controller
simulation
