摘要
研究并设计了智能旋翼振动控制实验的方案,对应用于智能旋翼小翼的闭环控制实验所需软硬件系统进行详细研究。分析讨论了采用本控制系统方案的可行性,确立使用AVRAtmega128单片机为核心的小翼控制系统平台的构建方案,进行了使用单片机为核心的控制方法设计,编写了相关控制程序。本试验系统相关特性适用于智能旋翼振动控制。
This paper briefed the control system built for the purpose of smart rotor vibration control.A control plan was given,system study has been done to settle the feasibility of the control structure for the rotor structure with the use of AVR atmega128 MCU.Software used in host and slave computers for the purpose of communication has been programmed,and the control design structure was given.
出处
《直升机技术》
2012年第1期46-51,共6页
Helicopter Technique
