Multivariable Control of Residual-Affected HCCI Engines Based on Model Predictive Control

Dinggen Li, Dingding Wang
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引用次数: 4

Abstract

A two-input and two-output physical model for pressures and combustion phases was built to realize the coordinated control of the peak pressures and combustion phases for a homogeneous charge compression ignition (HCCI) engine. This model is based on the Shaver' residual-affected HCCI engine model with the constant wall temperature heat transfer model suitable for HCCI combustion. A cooperative control system of pressure and combustion phase was designed using the model predictive control (MPC) theory with the variable valve timing (VVT) as the control method. The coordinated simulation experiment was done by using GT-Power and Matlab/Simulink. The results show that the control model satisfies the engine control demand, realizes the collaborative control of the pressure and combustion phase with control accuracies of ±30 kPa and ±0.6° CA, and the response time of 6-7 engine cycles.
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基于模型预测控制的残差影响HCCI发动机多变量控制
为实现均质装药压缩点火(HCCI)发动机峰值压力和燃烧相的协调控制,建立了压力和燃烧相的双输入双输出物理模型。该模型是在Shaver残余影响HCCI发动机模型的基础上建立的,采用了适用于HCCI燃烧的恒壁温度传热模型。采用模型预测控制(MPC)理论,以可变配气正时(VVT)为控制方法,设计了压力与燃烧相的协同控制系统。利用GT-Power和Matlab/Simulink进行了协同仿真实验。结果表明,该控制模型满足发动机控制需求,实现了压力和燃烧相位的协同控制,控制精度为±30 kPa和±0.6°CA,响应时间为6 ~ 7个发动机循环。
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