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2013 International Conference on Process Control (PC)最新文献

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Virtual model of an electro-hydraulic system 电液系统的虚拟模型
Pub Date : 2013-06-18 DOI: 10.1109/PC.2013.6581422
A. Kopčeková, M. Kopček, T. Skulavik
This paper deals with the design of model of electro-hydraulic system with failure simulation feature. The fundamental causes and effects of failures of electro-hydraulic system are summarized. Virtual Simulink model of electro-hydraulic system has been developed and implemented in compliance with performed FMEA (Failure Mode and Effects Analysis). Subsequent experimental part focuses to the simulation of selected failures on electro-hydraulic system model. The results of simulation of failures are shown in time response characteristics of monitored variables.
本文研究了具有故障仿真特征的电液系统模型的设计。总结了电液系统故障的基本原因和影响。基于FMEA (Failure Mode and Effects Analysis,失效模式与影响分析),开发并实现了电液系统的虚拟Simulink模型。随后的实验部分重点对电液系统模型上选取的故障进行了仿真。故障模拟的结果体现在被监测变量的时间响应特性上。
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引用次数: 1
Airship aerodynamics - Modeling principle of the aerodynamic forces by PEM method 飞艇空气动力学。气动力的PEM方法建模原理
Pub Date : 2013-06-18 DOI: 10.1109/PC.2013.6581377
F. Jelenciak, M. Gerke, I. Masár
This article describes a Projection Equivalent Method (PEM) as a new approach for modeling of aircraft. PEM is a method [20] by which it is possible to obtain a mathematical model of the aerodynamic forces and moments acting on the flying machine during flight. For PEM, it is characteristic that in principle it provides an acceptable regression model of aerodynamic forces and moments, which possesses a reasonable and plausible behavior from dynamics viewpoint. The main advantage of the PEM is that it is not necessary to carry out measurements in wind tunnel for identification of model parameters. Plausible dynamic behavior of the model can be achieved by specific correction parameters, which are possible to be determined on the base of experimental data obtained during a flight of the aircraft. In this article, we present the Projective Equivalent Method, which is applied to an airship. The airship is a special flight system, which is extremely sensitive to the aerodynamic forces impact. Therefore an airship is a suitable object for the comparison of a flight mechanics model providing data calculated by PEM and sensor data from experimental flight.
本文介绍了一种新的飞机建模方法——投影等效法(PEM)。PEM是一种方法[20],通过它可以获得飞行过程中作用在飞行器上的气动力和力矩的数学模型。PEM的特点是,它在原则上提供了一个可接受的气动力和力矩的回归模型,从动力学的角度来看,它具有合理和可信的行为。PEM的主要优点是不需要在风洞中进行模型参数识别的测量。模型的动力学行为可以通过特定的修正参数来实现,这些修正参数可以根据飞机飞行过程中获得的实验数据来确定。本文提出了一种适用于飞艇的投影等效方法。飞艇是一种特殊的飞行系统,对气动力的冲击极为敏感。因此,飞艇是一个比较飞行力学模型的合适对象,该模型提供了PEM计算数据和实验飞行的传感器数据。
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引用次数: 1
On pole placement LMI constraints in control design for linear discrete-time systems 线性离散系统控制设计中的极点放置LMI约束
Pub Date : 2013-06-18 DOI: 10.1109/PC.2013.6581385
D. Krokavec, A. Filasová
The paper addresses the problem of constrained pole placement control for discrete-time linear systems. Sufficient conditions for feasibility are outlined in terms of linear matrix inequalities for a D-stable circular region in the complex ś plain. In addition, in the case of state-space control, it is proven that by this way formulated pole placement problem is equivalently uttered using an quadratic integral state constraint, being added to Lyapunov function. Finally, the proposed principle is expanded for systems with polytopic uncertainties.
研究了离散线性系统的约束极点配置控制问题。用线性矩阵不等式的形式给出了复平面上d稳定圆区域的可行性的充分条件。此外,在状态空间控制的情况下,证明了用二次积分状态约束等效地表达了公式化的极点布置问题,并将其添加到Lyapunov函数中。最后,将该原理扩展到具有多面体不确定性的系统。
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引用次数: 15
Identification and self-tuning predictive control of heat exchanger 热交换器辨识与自整定预测控制
Pub Date : 2013-06-18 DOI: 10.1109/PC.2013.6581412
V. Bobál, M. Kubalcik, P. Dostál
Heat exchange belongs to the class of basic thermal processes which occur in a range of industrial technologies, particularly in the energetic, chemical, polymer and rubber industry. The process of heat exchange is often implemented by through-flow heat exchangers. It is apparent that for an exact theoretical description of dynamics of heat exchange processes it is necessary to use partial differential equations. Heat exchange is namely a process with distributed parameters. It is also necessary to take into account its nonlinear and stochastic character. In spite of these facts, most of thermal equipment is controlled by digital modifications of PID controllers at present. This paper deals with identification of a dynamic behavior of a through-flow heat exchanger and a design of an self-tuning predictive controller for its control. The designed controller was verified by a real-time control of experimental laboratory heat exchanger.
热交换属于发生在一系列工业技术中的基本热过程,特别是在能源、化学、聚合物和橡胶工业中。换热过程通常采用通流式换热器。很明显,要对热交换过程的动力学进行精确的理论描述,必须使用偏微分方程。换热是一个具有分布参数的过程。同时也要考虑到它的非线性和随机性。尽管如此,目前大多数热工设备都是通过PID控制器的数字修改来控制的。本文研究了通流换热器动态特性的辨识及自整定预测控制器的设计。通过对实验室换热器的实时控制,验证了所设计的控制器的有效性。
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引用次数: 12
期刊
2013 International Conference on Process Control (PC)
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