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作 者:曹灿 舒文君 于兵[1] CAO Can;SHU Wenjun;YU Bing(College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China)
机构地区:[1]南京航空航天大学能源与动力学院,江苏南京210016
出 处:《自动化仪表》2018年第5期44-47,共4页Process Automation Instrumentation
摘 要:随着导弹、火箭等特殊飞行器的机动性需求日益提高,矢量推力控制技术变得十分重要。但矢量推力机电作动系统是高阶、大惯量对象,因此其控制器参数的整定较为困难,且整定效果往往不够理想。针对上述问题,考虑到粒子群优化(PSO)算法全局寻优能力强、算法简单、易于实现等特点,采用PSO算法来优化控制器参数(控制增益)。对典型的飞行器矢量推力机电作动系统进行了研究,并建立了其数学模型。将控制增益整定等效为优化问题,采用PSO算法优化控制器参数。对优化后的矢量推力机电作动控制系统进行仿真,结果表明,该闭环系统单位阶跃响应的调节时间小于1 s、超调量为0.505%,同时喷管转动可以快速且准确地跟踪位置指令信号。仿真结果表明,优化后的控制器对该作动系统的控制效果良好,也验证了应用PSO算法解决控制优化问题的可行性。With the increasing demand for maneuverability of special aircrafts,such as missiles and rockets,thrust vector controltechnology has become more and more important.However,the thrust vector electromechanical actuation system is a high order objectwith large inertia,so the tuning of the parameters of its controller is very difficult,and the control effect is often not ideal.In view ofthe problems above,considering the particle swarm optimization(PSO) algorithm features strong capability of global optimization,simple and easier to implement,thus the PSO algorithm is adopted to optimize parameters of controller (control gain).Firstly,thetypical thrustvectorsystem with electromechanical actuator is researched,and its mathematical model is setup.Then,the control gaintuning is equivalent to optimization problem,the control parameters are optimized by using PSO algorithm. Simulation of theoptimized thrust vector controlsystem is carried out,and the results show that settling time of unit step response is less than 1 s,with0.505% overshoot,while nozzle position tracks the command signal quickly and accurately.This indicates the good control effect ofoptimized controller and verifies the feasibility of applying PSO to solve the problem of controller optimization.
关 键 词:矢量推力系统 机电作动器 PSO 控制增益 参数优化
分 类 号:TH13[机械工程—机械制造及自动化] TP23[自动化与计算机技术—检测技术与自动化装置]
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