基于云台式PGK的反旋翼筒控制系统设计及仿真  

Design and Simulation of Anti-Rotor Airfoil Control System Based on Cloud-Top PGK

作　　者：张刘帅 杨新民[1] 赵坤[1] ZHANG Liushuai;YANG Xinmin;ZHAO Kun(Transient State Key Laboratory,Nanjing University,Nanjing 210094,China)

机构地区：[1]南京理工大学瞬态国家重点实验室

出　　处：《兵器装备工程学报》2019年第12期95-99,共5页Journal of Ordnance Equipment Engineering

摘　　要：为了实现对云台式PGK的反旋翼筒可以在惯性空间下保持静止,设计了一种新型的控制系统,系统对反旋翼筒控制采用相位环+速度环+电流环三闭环的控制方法,并基于Matlab/Simulink对反旋翼筒的三闭环控制方法进行了仿真验证。仿真结果表明:采用该控制方法,反旋翼筒动静态性能良好,稳定性高,响应速度快。验证了此控制方案的可靠性,为项目的进行一步推进打下良好的基础。In order to realize that the anti-rotation wing of the cloud-top PGK can be kept still in the inertial space,a new control system was designed.The system used the phase loop+speed loop+current loop three closed loop control method for the anti-rotary wing control,and was based on Matlab/Simulink to simulate the three closed-loop control methods of the anti-rotary wing.The simulation results show that the control method has good dynamic and static performance,high stability and fast response speed.It verified the reliability of this control scheme and laid a good foundation for the project to advance step by step.

关 键 词：MATLAB/SIMULINK 三闭环 云台式PGK 反旋翼筒 

分 类 号：TP13[自动化与计算机技术—控制理论与控制工程]