摘要
本文设计了一种无人机用分布式电动舵机,主要采用RS-422总线和分布式布局的设计思路,完成了控制电路、功率放大电路、执行机构和控制软件的设计。同时,通过多学科的联合仿真及试验验证,证明该电动舵机设计方案的合理性和可行性,以满足无人机对电动舵机的需求。
In this paper,a distributed electric actuator for UAV was designed.The control circuit,power amplifier circuit,actuator and control software were designed by using RS-422 bus and distributed layout.At the same time, through multi-disciplinary joint simulation and experimental verification,the rationality and feasibility of the design scheme of the electric actuator were proved to meet the requirements of the UAV for the electric actuator.
作者
冉令峰
RAN Lingfeng(China Institute of Air-to-air Missile,Luoyang Henan 471000)
出处
《河南科技》
2019年第8期56-58,共3页
Henan Science and Technology
关键词
无人机
分布式
电动舵机
联合仿真
UAV
distributed
electro actuator
joint simulation
