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2015 23rd Mediterranean Conference on Control and Automation (MED)最新文献

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Set-based direct visual servoing for nanopositioning 基于集合的纳米定位直接视觉伺服
Pub Date : 2015-06-16 DOI: 10.1109/MED.2015.7158839
Zhichao Liu, Jianliang Wang, E. Poh
Atomic force microscopy (AFM) can be used as an image tool in nanoscale for nanopositioning and other similar works. This problem can be seen as a visual servoing problem. Traditional works for this problem use position-based algorithms, however, the correspondence problem is needed to be solved by feature matching and tracking firstly, as a prerequisite for vision-based control. The correspondence problem refers to the problem of ascertaining which parts of one image correspond to which parts of another image. To solve the problem of AFM based nanomanipulations, we present a novel set-based direct visual servoing controller (SDVSC) for nanopositioning that is based on the whole gray image and does not require feature matching and tracking.
原子力显微镜(AFM)可以用作纳米尺度的成像工具,用于纳米定位和其他类似工作。这个问题可以看作是视觉伺服问题。传统的算法采用基于位置的算法,但首先需要通过特征匹配和跟踪来解决对应问题,这是实现基于视觉控制的前提。对应问题是指确定一个图像的哪些部分对应于另一个图像的哪些部分的问题。为了解决基于AFM的纳米定位问题,提出了一种基于整幅灰度图像且不需要特征匹配和跟踪的基于集的纳米定位直接视觉伺服控制器(SDVSC)。
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引用次数: 0
Combined stochastic and deterministic interval predictor for time-varying systems 时变系统的随机与确定性组合区间预测器
Pub Date : 2015-06-16 DOI: 10.1109/MED.2015.7158849
J. M. Bravo, T. Alamo, M. E. Gegúndez, D. Marín
This work proposes a new interval predictor for time-varying linear systems. An interval predictor is a method that provides an interval as outer estimation of the future system output. The center of the interval prediction can be used as point or nominal prediction. This interval center is obtained by a linear combination of stored past outputs. The interval width is obtained using an outer bound of the prediction error. Two different approaches have been considered in literature, based on deterministic and stochastic assumptions respectively. The novelty of this work is to use a combined deterministic and stochastic assumption on this bound to obtain the interval prediction. The aim is to achieve a low error in the central prediction and a small interval width. An example is provided to illustrate the improvement provided by the proposed predictor.
本文提出了一种新的时变线性系统区间预测器。区间预测器是一种提供区间作为未来系统输出的外部估计的方法。区间预测的中心可用作点预测或标称预测。这个间隔中心是由存储的过去输出的线性组合得到的。区间宽度由预测误差的外边界得到。文献中考虑了两种不同的方法,分别基于确定性和随机假设。本文的新颖之处在于对该界使用确定性和随机相结合的假设来获得区间预测。其目的是使中心预测误差小,区间宽度小。给出了一个例子来说明所提出的预测器所提供的改进。
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引用次数: 2
Control of disturbed systems with measurement delays: Application to quadrotor vehicles 具有测量延迟的扰动系统控制:在四旋翼飞行器上的应用
Pub Date : 2015-06-16 DOI: 10.1109/MED.2015.7158877
R. Sanz, P. Garcia, Qing-Chang Zhong, P. Albertos
Disturbances and uncertainties make very difficult the control of Unmanned Aerial Vehicles (UAV). The problem is even worse, if delays are involved in the process. The uncertainty and disturbance estimator (UDE) is a technique based on the idea that the unknown dynamics and disturbances of a system can be accurately approximated by passing them through a filter with the appropriate bandwidth. This makes it very easy to design and tune a controller to deal with uncertainties and disturbances. But this solution is very sensitive to time delays. In this paper, this strategy is further developed for systems with measurement delays and hence the range of systems for which it can be applied is broadened.
干扰和不确定性给无人机的控制带来了很大的困难。如果在这个过程中出现延迟,问题就更糟了。不确定性和干扰估计器(UDE)是一种基于这样一种思想的技术,即系统的未知动态和干扰可以通过具有适当带宽的滤波器精确地逼近。这使得设计和调整控制器来处理不确定性和干扰变得非常容易。但是这种解决方案对时间延迟非常敏感。在本文中,该策略被进一步发展为具有测量延迟的系统,从而扩大了它可以应用的系统范围。
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引用次数: 1
Experimental investigation of nonlinear controllers applied to a 3DOF hover: SMC via ALQR approach 基于ALQR方法的三维悬停SMC非线性控制器实验研究
Pub Date : 2015-06-16 DOI: 10.1109/MED.2015.7158800
R. L. Pereira, K. Kienitz
This paper presents an application of sliding mode controllers obtained via amplified linear quadratic regulator (ALQR) strategy to a hover with three degrees of freedom. The purpose of the designed control system is to track reference trajectories and ensure performance and stability in spite of disturbance, noise and unmodeled dynamics. Simulations were performed using MATLAB/Simulink in order to verify/compare the performance of the nonlinear controllers proposed. For validation of the algorithm a didactic plant (3DOF Hover) was chosen produced by Quanser Consulting, that simulates typical behaviors of an VTOL (“vertical taking-off landing”) aircraft, also known as X4-flyer. The dynamic of the hover can be described by a 6th order model taking as state variables the angles of yaw, pitch, roll and associated rates. The experiments showed that designed nonlinear controllers using sliding mode control via ALQR are robust to noises and for a range of unmodeled nonlinearities.
本文提出了一种由放大线性二次型调节器(ALQR)策略获得的滑模控制器在三自由度悬停飞行器上的应用。所设计的控制系统的目的是跟踪参考轨迹,并确保在干扰、噪声和未建模的动态情况下的性能和稳定性。利用MATLAB/Simulink进行仿真,验证/比较所提出的非线性控制器的性能。为了验证该算法,我们选择了一个由Quanser咨询公司生产的教学工厂(3DOF Hover),该工厂模拟了垂直起降飞机(也称为x4飞行器)的典型行为。悬停动力学可以用以横摆角、俯仰角、横摇角和相关速率为状态变量的六阶模型来描述。实验表明,采用ALQR滑模控制设计的非线性控制器对噪声和一系列未建模的非线性具有较强的鲁棒性。
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引用次数: 6
Identification of flexible wing aircraft models using hyperbolic metrics 用双曲度量法辨识柔性翼飞机模型
Pub Date : 2015-06-16 DOI: 10.1109/MED.2015.7158848
A. Soumelidis, Z. Szabó, P. Seiler, Abhineet Gupta, J. Bokor
This paper proposes a novel discrete time identification method for flexible wing aircraft models from simulated data. The special properties of the dynamics arise from the fact that all the poles are located very close to the unit circle and their location changes with the flight velocity. Using identification criteria based on Euclidean metrics suffers from the problem of obtaining instability in the search and also on the possible high number of poles. The paper offers an alternative approach and associated identification method to obtain the poles directly using Laguerre-representation of the impulse responses and hyperbolic metrics for identification criteria. The method utilises the hyperbolic geometrical properties of the descriptions of discrete-time signals and systems on the unit disc, and is strictly connected to the representations in rational orthogonal bases. Beyond the conceptual clarity, examples also confirm that it forms an adequate basis for estimating poles of systems as a significant part of an identification process.
提出了一种基于仿真数据的柔性翼飞机模型离散时间识别方法。这种特殊的动力学性质是由于所有极点都非常靠近单位圆,并且它们的位置随飞行速度的变化而变化。使用基于欧几里得度量的识别准则存在搜索不稳定的问题,同时也存在极数可能过高的问题。本文提供了一种替代方法和相关的识别方法,直接使用脉冲响应的拉盖尔表示和双曲度量作为识别准则来获得极点。该方法利用离散时间信号和系统在单位圆盘上描述的双曲几何性质,并与有理正交基的表示严格相连。除了概念的明确性之外,实例也证实,它构成了估计系统极点的充分基础,是识别过程的一个重要部分。
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引用次数: 1
An algorithm with low computational requirements to constrain the Shapley value in coalitional networks 一种低计算量约束联合网络Shapley值的算法
Pub Date : 2015-06-16 DOI: 10.1109/MED.2015.7158900
F. J. Muros, J. Maestre, E. Algaba, T. Alamo, E. Camacho
In this paper, we deal with a distributed control scheme for linear systems in which the local controllers work cooperatively whenever the benefits from a control perspective are higher than the corresponding communication requirements. To this end, the network topology may vary with time so that all the communication links with a minor contribution to the overall performance are disconnected. Hence, there is also a change in the overall control law, which must be adapted to the information flows enabled by the network topology. This whole framework can be modeled as a cooperative game, which allows us to apply tools such as the Shapley value to gain an insight into the distributed control problem. In particular, we show an alternative way to impose restrictions on this value by using a more computationally efficient design procedure.
在本文中,我们讨论了线性系统的分布式控制方案,当从控制角度的收益高于相应的通信要求时,本地控制器就会协同工作。为此,网络拓扑可能会随着时间的变化而变化,从而断开对整体性能贡献较小的所有通信链路。因此,总体控制律也发生了变化,必须适应网络拓扑所支持的信息流。整个框架可以建模为合作博弈,这允许我们应用Shapley值等工具来深入了解分布式控制问题。特别是,我们展示了另一种方法,通过使用计算效率更高的设计过程来对该值施加限制。
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引用次数: 4
MPC implementation in a PLC based on Nesterov's fast gradient method 基于Nesterov快速梯度法的MPC在PLC中的实现
Pub Date : 2015-06-16 DOI: 10.1109/MED.2015.7158777
M. Pereira, D. Limón, D. M. D. L. Peña, T. Alamo
This work presents a linear quadratic model predictive controller (MPC) implemented in an industrial programable logic controller (PLC). The control law is calculated by solving on-line the quadratic programming problem derived from the optimization control problem of MPC. Nesterov's fast gradient algorithm has been used to solve the corresponding linear quadratic MPC problems with input constraints. The predictive controller has been implemented in a Schneider Electric M340 using the standard structured language from the IEC 1131.1 norm. The memory and computational time requirements of the proposed implementation have been characterized through extensive simulations. In addition, the properties of the proposed controller have been experimentally demonstrated using a test-bed in which the MPC running in the M340 controls a model of a quadruple-tank process simulated in Matlab/Simulink through an OPC server.
本文提出了一种在工业可编程逻辑控制器(PLC)中实现的线性二次模型预测控制器(MPC)。通过在线求解由MPC优化控制问题导出的二次规划问题来计算控制律。Nesterov的快速梯度算法已被用于求解相应的具有输入约束的线性二次型MPC问题。该预测控制器已在施耐德电气M340中使用来自IEC 1131.1规范的标准结构化语言实现。所提出的实现的内存和计算时间需求已经通过广泛的模拟进行了表征。此外,所提出的控制器的特性已经通过实验验证,在M340中运行的MPC控制通过OPC服务器在Matlab/Simulink中模拟的四缸过程模型。
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引用次数: 6
A Future Internet interface to control programmable networks 用于控制可编程网络的未来Internet接口
Pub Date : 2015-06-16 DOI: 10.1109/MED.2015.7158757
S. Battilotti, Federico Cimorelli, R. Cusani, F. D. Priscoli, C. Giorgi, V. Suraci, L. Zuccaro
current internet infrastructure is still configured and managed manually or adopting a limited level of automation. The Future Internet aims to provide the network resources as a service to ease the process of automatic designing, controlling and supervising the telecommunication infrastructure. A key enabler of the Future Internet is the virtualization of the available resources and of the related functionalities. The widespread of cloud computing, Software Defined Network (SDN) and Network Function Virtualization (NFV) technologies opened the way for a total control of programmable networks. Many open and commercial implementations have adopted this paradigm, but they expose a fragmented set of dissimilar interfaces that often offer similar or even overlapping functionalities. The result is that uncontrolled, open-loop routines and procedures still require a manual intervention. In this paper, we describe an open interface and its reference implementation, to control programmable networks adopting a novel, closed-loop approach based on end-users feedbacks. The proposed interface has been implemented as a Future Internet Generic Enabler named OFNIC.
当前的Internet基础设施仍然是手动配置和管理的,或者采用有限的自动化水平。未来互联网旨在将网络资源作为一种服务来提供,以简化电信基础设施的自动设计、控制和监督过程。未来因特网的一个关键促成因素是可用资源和相关功能的虚拟化。云计算、软件定义网络(SDN)和网络功能虚拟化(NFV)技术的广泛应用为可编程网络的全面控制开辟了道路。许多开放和商业实现都采用了这种范例,但是它们暴露了一组零散的不同接口,这些接口通常提供相似甚至重叠的功能。结果是,不受控制的开环例程和程序仍然需要人工干预。在本文中,我们描述了一个开放接口及其参考实现,采用一种基于最终用户反馈的新颖闭环方法来控制可编程网络。提出的接口已被实现为未来互联网通用使能器OFNIC。
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引用次数: 3
Optimal design and modeling of a tilt wing aircraft 倾斜翼飞机的优化设计与建模
Pub Date : 2015-06-16 DOI: 10.1109/MED.2015.7158828
A. Lindqvist, Emil Fresk, G. Nikolakopoulos
The aim of this article is to present an optimal model for the behavior of a tilt wing aircraft during its transition state. A tilt wing aircraft is a hybrid between a helicopter and a plane, which has the capabilities of both parts, meaning that it can stand still and hover and by tilting its wing 90 degrees to act like a regular plane. Overall, a tilt wing aircraft has the extended merits of vertical take offs and landings, to stand still and hover in mid air, while being able to travel in long distances efficiently. The novelty of this article stems from: a) the analysis of the aircraft during the transition between helicopter mode and plane for the angles between 0-90 degrees, b) the comparison between the model extracted from the simulations and tests from a wind tunnel for the wing, and c) the proposal for an optimal design for a tilt wing UAV. The efficiency of the proposed modeling approach has been evaluated in multiple simulated and experimental verification.
本文的目的是为倾斜翼飞机在过渡状态下的行为提出一个最佳模型。倾斜翼飞机是一种介于直升机和飞机之间的混合体,它具有两部分的能力,这意味着它可以静止不动,悬停,并通过将机翼倾斜90度来像普通飞机一样飞行。总的来说,倾斜机翼飞机具有垂直起降的扩展优点,可以在半空中静止和悬停,同时能够有效地进行长距离飞行。本文的新颖之处在于:a)分析了飞机在直升机模式和飞机之间的0-90度角转换过程,b)将机翼的模拟模型与风洞试验模型进行了比较,c)提出了倾斜翼无人机的优化设计方案。通过多次仿真和实验验证,对所提建模方法的有效性进行了评价。
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引用次数: 7
Real-time estimation of thermal comfort indices in an office building with a solar powered HVAC system 太阳能暖通空调办公大楼热舒适指数的实时估算
Pub Date : 2015-06-16 DOI: 10.1109/MED.2015.7158844
Mario L. Ruz, S. Fragoso, David Rodriguez, F. Vázquez
This paper presents an interactive software tool to monitor in real-time thermal comfort in buildings. Specifically, the tool is used to estimate predicted mean vote (PMV) and predicted percentage dissatisfied (PPD) indices, which are widely accepted in the framework of thermal comfort and recognized by international standards. In this work, the tool was tested in an office building with an HVAC system based on solar energy. To perform this task, a network architecture that enables communication between different protocols is proposed, with a TCP/IP-Modbus gateway and a web server as the main elements, providing in this way external connectivity and data collection from different sensors. The tool communicates remotely with the renewable system and proposes corrective control indications to maintain the indoor-air conditions inside the optimal comfort range.
本文介绍了一种用于实时监测建筑热舒适性的交互式软件工具。具体而言,该工具用于估计预测平均投票(PMV)和预测不满意百分比(PPD)指数,这在热舒适框架中被广泛接受,并为国际标准所认可。在这项工作中,该工具在一个基于太阳能的暖通空调系统的办公大楼中进行了测试。为此,提出了一种支持不同协议间通信的网络架构,以TCP/IP-Modbus网关和web服务器为主要元素,以这种方式提供外部连接和不同传感器的数据采集。该工具与可再生系统进行远程通信,并提出纠正控制指示,以保持室内空气条件在最佳舒适范围内。
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引用次数: 2
期刊
2015 23rd Mediterranean Conference on Control and Automation (MED)
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