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民用涡扇发动机多变量增广LQR控制器设计
引用本文:王骥超,郭迎清.民用涡扇发动机多变量增广LQR控制器设计[J].航空计算技术,2014(5):31-33.
作者姓名:王骥超  郭迎清
作者单位:西北工业大学动力与能源学院,陕西西安,710072
摘    要:针对民用涡扇发动机设计多变量控制器,提出将多变量增广LQR控制算法引入到民用涡扇发动机的方法。将发动机控制量作为增广的状态向量引入LQR算法设计,并根据控制系统回路的性能需求,设计期望动态响应曲线;期望动态响应与实际动态响应的差值范数作为优化目标用来调整、确定LQR控制算法的权阵取值;设计的控制器与民用涡扇发动机非线性模型仿真验证。结果表明,多变量增广LQR控制器满足民用涡扇发动机的控制需求。

关 键 词:民用涡扇发动机  多变量控制  增广最优二次型控制器  权值选取

Design of Multi-variable Augmented LQR Controller for Civil Aero-engine
WANG Ji-chao,GUO Ying-qing.Design of Multi-variable Augmented LQR Controller for Civil Aero-engine[J].Aeronautical Computer Technique,2014(5):31-33.
Authors:WANG Ji-chao  GUO Ying-qing
Institution:(School of Power and Energy,Northwestern Polytechnical University,Xi'an 710072, China)
Abstract:This paper introduces a multivariable augmented LQR controller to a civil aero-engine control . The control variables are used as augmented states in this control algorithm .And an expected response curve is designed ,according to the engine performance requirements .The difference between expected dy-namic response and actual dynamic response is served as the optimization objective function .By optimi-zing this target function ,a pair of optimal LQR weights is found .Finally,simulation proves that the con-troller is able to control the civil aero-engine.
Keywords:Civil aero-engine  multivariable control  augmented LQR controller  choosing LQR weighting
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