论文部分内容阅读
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。
The scheme of intelligent rotor vibration control experiment is researched and designed. The hardware and software system required for the closed-loop control experiment of the intelligent rotor wing is studied in detail. The feasibility of using this control system is analyzed and discussed. The establishment of the control system platform using AVRAtmega128 microcontroller as its core is established. The control method design using SCM as the core is analyzed and the relevant control program is compiled. The test system related features apply to intelligent rotor vibration control.