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Control of a two-stage turbocharged diesel engine air path system for mode transition via feedback linearization

机译:通过反馈线性化控制用于模式转换的两级涡轮增压柴油机空气路径系统

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This paper presents a nonlinear control design for a Diesel engine air path system with a two-stage turbocharger. The proposed design aims at improving the robustness and smoothness of the system response during mode transitions, namely by coordinating the available actuators to regulate the intake and exhaust manifold pressures and air mass flow rate to specified set points. A feedback linearization method is applied for the control design, based upon a simplified control-oriented air path system model. A formal stability proof of the zero dynamics is conducted to justify the selection of the appropriate system outputs and of the nonlinear control technique adopted in this study. To address model uncertainties and saturation issues for the actuators, the proposed controller is implemented using an internal model control structure. The proposed control scheme is then evaluated in simulation, using a high-fidelity engine model. Verification is conducted considering two case studies, first a simple load transient profile including a mode transition for the two-stage turbocharger, and then a portion of driving cycle.
机译:本文提出了一种带有两级涡轮增压器的柴油机风道系统的非线性控制设计。提出的设计旨在提高模式转换期间系统响应的鲁棒性和平滑度,即通过协调可用的执行器来将进气和排气歧管压力以及空气质量流量调节到指定的设定点。基于简化的面向控制的风道系统模型,将反馈线性化方法应用于控制设计。进行了零动力学的形式稳定性证明,以证明选择适当的系统输出和本研究采用的非线性控制技术的合理性。为了解决执行器的模型不确定性和饱和问题,使用内部模型控制结构来实现所提出的控制器。然后使用高保真引擎模型在仿真中评估提出的控制方案。考虑两个案例研究进行验证,首先是简单的负载瞬态曲线,包括两级涡轮增压器的模式转换,然后是行驶周期的一部分。

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