悬停状态电控旋翼桨距控制  

Study on the blade pitch control of electrically controlled rotor in hover

作　　者：夏鹤鸣[1] 陆洋[1] 

机构地区：[1]南京航空航天大学直升机旋翼动力学国家级重点实验室,南京210016

出　　处：《航空动力学报》2009年第10期2213-2220,共8页Journal of Aerospace Power

基　　金：国家自然科学基金(50805074);航空创新基金(08A52001)

摘　　要：针对改进型电控旋翼系统,首先建立了其各控制环节的数学模型,采用串级PID(proportion in-tegration differentiation)控制算法设计了悬停状态下电控旋翼桨距控制律,PID参数根据Ziegler-Nichols方法进行整定.通过仿真计算分析,初步验证了该控制算法对于桨距控制的有效性.以上述控制方法为基础,进一步开展了悬停状态下电控旋翼桨距控制的闭环试验研究,成功的实现了电控旋翼桨距幅值和相位的控制,验证了串级PID电控旋翼桨距控制算法的正确性和有效性.In order to control the blade pitch of the electrically controlled rotor(ECR) accurately,the mathematic models of every part of the ECR system were built based on the improved ECR system.Then the cascade proportion integration differentiation(PID) control method was introduced to design the control law for the blade pitch of ECR in hover based on the mathematic models,and the PID parameters were tuned with the Ziegler-Nichols method.The results of the simulation analysis verified preliminarily the effective...

关 键 词：电控旋翼 桨距 仿真 控制系统 

分 类 号：V249[航空宇航科学与技术—飞行器设计]