1,721,091 research outputs found

    Preface

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    This book, published in two volumes, embodies the proceedings of the 15th European Workshop on Advanced Control and Diagnosis (ACD 2019) held in Bologna, Italy, in November 2019. It features contributed and invited papers from academics and professionals specializing in an important aspect of control and automation. The book discusses current theoretical research developments and open problems and illustrates practical applications and industrial priorities. With a focus on both theory and applications, it spans a wide variety of up-to-date topics in the field of systems and control, including robust control, adaptive control, fault-tolerant control, control reconfiguration, and model-based diagnosis of linear, nonlinear and hybrid systems. As the subject coverage has expanded to include cyber-physical production systems, industrial internet of things and sustainability issues, some contributions are of an interdisciplinary nature, involving ICT disciplines and environmental sciences. This book is a valuable reference for both academics and professionals in the area of systems and control, with a focus on advanced control, automation, fault diagnosis and condition monitoring

    Residual generator design for linear dynamic system fault detection

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    This paper investigates few minor new results regarding the computation of residual generator functions in order to realise for example complete diagnosis schemes in linear multivariable systems with additive faults and disturbances. The use of canonical input-output polynomial forms leads to characterise in a straightforward fashion the basis of the subspace described by all the possible residual generators. These tools show how the mathematical description of these filters can be obtained also by following a black-box identification approach

    Estimation of the Power Coefficient Map for a Wind Turbine Simulated Benchmark

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    Since the energy generation capacity of installed wind turbine is increasing, the interest in optimising the efficiency of these wind turbines is growing, as well. The optimal operating points for the power and speed control of the turbines depends on a mapping to the power conversion ratio from tip speed ratio and blade pitch angles. This mapping usually is not known in analytical form, but in general represented by approximated two–dimensional maps (i.e. look–up tables). Another issue can derive from the accuracy of the map itself. It might be correct but uncertain. The main problem of the methods available in the literature is that the power conversion ratio is represented as two–dimensional map. Therefore, this paper suggests a scheme to estimate this power conversion ratio in an analytical form, described as two–dimensional polynomial, whose degree has to be optimised as well. This estimated analytical relation can subsequently be used to design optimal controller, as well as for robust fault diagnosis applications

    Residual function design for linear multivariable systems

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    Classical model–based fault detection schemes for linear multivariable systems require the definition of suitable residual functions. This paper shows the possibility of identifying residual generators even when the system model is unknown, by following a black–boxapproac h. The result is obtained by using canonical input–output polynomial forms which lead to characterise in a straightforward fashion the basis of the subspace described by all possible residual generators. The performance of the proposed identification method is tested by means of a Monte Carlo simulation

    Active Fault Tolerant Control Scheme for a General Aviation Aircraft Model

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    This paper addresses the development of a novel active fault tolerant control scheme. The methodology is based on a fault detection and diagnosis procedure relying on adaptive filters designed via the nonlinear geometric approach. The controller reconfiguration exploits a further control loop, depending on the on-line estimate of the fault signal. One of the advantages of this strategy is that, for example, a structure of logic–based switching controller is not required. The active fault tolerant control scheme is therefore applied to a PA–30 aircraft simulator in several flight conditions, in the presence of actuator faults, turbulence, measurement noise, and modelling errors. The achieved results in faulty conditions show the enhancement of the flying quality, the asymptotic fault accommodation, and the control objective recovery

    Neural networks for fault diagnosis and identification of industrial processes

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    In this work a model--based procedure exploiting analytical redundancy via state estimation techniques for the diagnosis of faults regarding sensors of a dynamic system is presented. Fault detection is based on Kalman filters designed in stochastic environment. Fault identification is therefore performed by means of different neural network architectures. In particular, neural networks are used as function approximators for estimating sensor fault sizes. The proposed fault diagnosis and identification tool is tested on a industrial gas turbine

    10th IFAC Symposium on Fault Detection, Supervision and Safety for Technical Processes : SAFEPROCESS 2018 : Warsaw, Poland, 29–31 August 2018 : PROCEEDINGS

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    Budapest (Hungary, 2000), Washington DC (USA, 2003), Beijing (China, 2006), Barcelona (Spain, 2009), Mexico City (Mexico, 2012), and Paris (France, 2015). The continuous increase in the complexity of modern industrial systems and objects as well as growing reliability demands regarding their operation and control quality are serious challenges for further development of the theory and practice of control and technical diagnostics. Early detection of faults is critical in avoiding performance degradation and damage to machinery or human life. The SAFEPROCESS symposium is a triennial meeting of IFAC and a major international gathering of leading experts in the academia and industry from all over the world. It aims at strengthening the contact between the academia and industry to build up new networks and cultivate existing relations. High-level speakers have gave talks on a wide spectrum of topics related to fault diagnosis, process supervision, safety monitoring and fault-tolerant control, as well as state-ofthe- art applications and emerging research directions. The symposium has been also a forum for young researchers, with the opportunity to present their scientific ambitions and work to an audience of international communities of technical diagnostics and control. Fault diagnosis and fault-tolerant control have developed into a major research area at the intersection of system and control engineering, applied mathematics and statistics or soft computing, as well as application fields such as mechanical, electrical, chemical and aerospace engineering. IFAC is recognized as playing a crucial role in this aspect by launching a triennial symposium dedicated to this subject. The program of SAFEPROCESS 2018 included 25 regular and 13 invited sessions in 5 parallel tracks. It also contained 3 plenary and 6 semi-plenary talks prepared by outstanding academic and industrial experts. We hope that those presentations gave the participants the opportunity to share in the knowledge and experience of worldrenowned scientists and experts in many exciting topics such as distributed fault diagnosis, integration of diagnosis and fault tolerant control, model-based fault diagnosis of wind turbines, model-free approaches to faulttolerant control, robust fault detection using setmembership approaches, as well as fault diagnosis needs and challenges in civil aircrafts

    Identification of residual generators for fault detection of linear dynamic models

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    Classical model-based fault detection schemes for linear multivariable systems require the definition of suitable residual functions. This paper shows the possibility of identifying residual generators even when the system model is unknown, by following a black-box approach. The result is obtained by using canonical input-output polynomial forms which lead to characterise in a straightforward fashion the basis of the subspace described by all possible residual generators. The performance of the proposed identification method is tested by means of Monte Carlo simulations

    Fault Diagnosis for Aircraft System Models

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    Safety in aircraft systems is a concern of rising importance, especially due to the sophisticated control devices exploited to improve the overall system performance, including both digital designs and complex hardware (input-output sensors, actuators, and components). Thus, control systems must include automatic supervision tasks to diagnose incipient malfunctions, as early as possible. This book focuses on the design of robust linear and nonlinear dynamic filters, obtained via model-based and analytical approaches for fault diagnosis and identification. The problem is treated in all its aspects covering: nonlinear modelling of aircraft systems; design of disturbance decoupled dynamic filters for residual generation; fault detection and estimation, fault tolerant control. Sample case studies are used to demonstrate the application of these techniques to high fidelity flight simulators. This book will be of interest to researchers in aircraft fault tolerant control, fault detection and diagnosis. Aircraft control engineers interested in applying the latest methods in fault detection and diagnosis will benefit from the simulation examples

    Approximation of Non--Linear System with Identified Hybrid Models

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    This paper addresses the identification of non-lineardynamic systems. A wide class of these systems canbe described using non-linear time-invariantregression models, that can be approximated by means of piecewise affine prototypes with an arbitrary degree of accuracy. This workconcerns the identification of piecewise affine model structure through input-output data acquired from a dynamic process. In order to show the effectiveness of the developed technique, the results obtained in the identification of both a simple simulated system and a real dynamic process are reporte
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