3 edition of Fault diagnosis and reconfiguration in flight control systems found in the catalog.
Fault diagnosis and reconfiguration in flight control systems
Includes bibliographical references and index.
|Statement||by Chingiz Hajiyev and Fikret Caliskan.|
|Series||Cooperative systems -- v. 2|
|LC Classifications||TL678 .H34 2003|
|The Physical Object|
|Pagination||xxvi, 342 p. :|
|Number of Pages||342|
|LC Control Number||2003060649|
3. Applications of fault diagnosis This paper took certain BNG aircraft flight control system of A/P(autopilot) operating abnormal failure data in the past three years as an example, classified fault phenomena and fault reasons, established Fuzzy Neural Network fault diagnosis model and locating pos itions of fault by using the model. and Caliskan covered the combined fault diagnosis and reconfiguration in flight control systems . In this study, first a Fault Detection and Isolation (FDI) based on the full-order UIO structure is presented. Then the accommodation technique is given. In the FDI approach, extra design freedom isFile Size: KB.
Fault Diagnosis and Fault-Tolerant Control and Guidance for Aerospace demonstrates the attractive potential of recent developments in control for resolving such issues as improved flight performance, self-protection and extended life of structures. Importantly, the text deals with a number of practically significant considerations: tuning, complexity of design, real-time capability, evaluation. control and self-repairing flight control systems be- gun in early s [38,39]. An early excellent work on the design issues for fault-tolerant aircraft control was given in . Other early (tutorial) papers on the subject of FTCS include [41,42,38,43]. More recently, fault-tolerant control has attracted more and more attention in both.
(A) S. Hansen, M. Blanke and J. Adrian. Diagnosis of UAV Pitot Tube Defects Using Statistical Change Detection. In proceedings of 7th Symposium on Intelligent Autonomous Vehicles, (B) S. Hansen and M. Blanke. Control Surface Fault Diagnosis for Small Au-tonomous Aircraft. In proceedings of 1st Australian Control Conference, Cited by: 1. [HC03] Chingiz Hajiyev and Fikret Caliskan, Fault Diagnosis and Reconfiguration in Flight Control Systems, Kluwer Academic Publishers, October , ISBN [ BKLS03 ] Mogens Blanke, Michel Kinnaert, Jan Lunze, Marcel Staroswiecki, Diagnosis and Fault-Tolerant Control, Springer-Verlag, August 1, , ISBN:
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The problems of fault detection, isolation, and reconfiguration in flight control systems are considered. These problems are main concerns of the book and are investigated in the following chapters. The problem of fault diagnosis and reconfigurable control is a new and actually developing field of science and engineering.
The subject becomes more interesting since there is an increasing demand for the navigation and control systems of aerospace vehicles, automated actuators etc.
to Cited by: The problem of fault diagnosis and reconfigurable control is a new and actually developing field of science and engineering. The subject becomes more interesting since there is an increasing demand for the navigation and control systems of aerospace vehicles, automated actuators etc.
to. Get this from a library. Fault diagnosis and reconfiguration in flight control systems. [Chingiz Hajiyev; Fikret Caliskan] -- "This is the first volume that involves reconfigurable control, which is the contemporary field of automatic control. Also, for the first time, fault diagnosis and reconfigurable control are combined.
Fault Diagnosis and Reconfiguration in Flight Control Systems Chingiz Hajiyev, Fikret Caliskan (auth.) The problem of fault diagnosis and reconfigurable control is a new and actually developing field of science and engineering. Free 2-day shipping. Buy Cooperative Systems: Fault Diagnosis and Reconfiguration in Flight Control Systems (Hardcover) at Fault Diagnosis and Reconfiguration in Flight Control Systems (Cooperative Systems) Pdf, Download Ebookee Alternative Effective Tips For A Best Ebook Reading.
This book provides readers with a design approach to the automatic flight control systems (AFCS). The AFCS is the primary on-board tool for long flight operations, and is the foundation for the airspace modernization initiatives.
In this text, AFCS and autopilot are employed interchangeably. Fault Diagnosis and Reconfiguration in Flight Control Systems Cooperative Systems: : Hajiyev, Chingiz: Libros en idiomas extranjerosAuthor: Chingiz Hajiyev.
Self-repairing Flight Control Systems 9 Fault Detection and Dynamic Reconfiguration 10 Analytical Redundancy 11 Game Theory and Real-time Parameter Insensitive Disturbance Attenuating Redesign 12 Techniques for Reconfiguration 12 Sensor/Actuator Fault Diagnosis 17 Sensor Fault Detection in Flight Control.
Control reconfiguration is an active approach in control theory to achieve fault-tolerant control for dynamic systems.
It is used when severe faults, such as actuator or sensor outages, cause a break-up of the control loop, which must be restructured to prevent failure at the system level. In addition to loop restructuring, the controller parameters must be adjusted to accommodate changed.
Fault diagnosis in dynamic systems via Kaiman filter innovation sequence, IFAC 14th World Congress, Beijing, China: – Google Scholar Hajiyev, Ch.
and Caliskan, F. ().Cited by: 3. Fault diagnosis and fault tolerant control strategies for aerospace systems Abstract: This work presents two active fault tolerant control systems for aerospace applications. The former case study regards an aircraft longitudinal autopilot and the latter one a satellite attitude control system, both in case of faults affecting the actuators.
Book Fault Diagnosis and Reconfiguration in Flight Control Systems Conference Paper Reconfigurable Fault-Tolerant UAV Flight Control Against Act. In this paper the application of the concepts of failure detection, fault diagnosis and dynamic reconfiguration to real time aircraft flight control systems is reviewed in detail.
Some new results concerning the sensitivity and insensitivity of observers and a new approach to reconfiguration of control laws are also : R. Vepa, F. Caliskan. Automatic Flight Control Systems - Latest Developments emphases on a selection of significant research areas, such as inertial navigation, control of unmanned aircraft and helicopters, trajectory control of an unmanned space re-entry vehicle, aeroservoelastic control, adaptive flight.
Chapter 2 focuses on a literature review about the fault-tolerant flight control systems already developed for aircraft. Chapter 3 presents the nonlinear model used for simulation and control design. Chapter 4 describes a new system for the detection and isolation of actuator faults in an by: Diagnosis and Failure Management of Flight Control Actuation Systems." The specific goals of this contract were twofold To assess the applicability of artificial intelligence methods and techniques to aircraft flight control system actuator real-time fault diagnosis and failure Size: 4MB.
A scheme for sensor online fault diagnosis and reconfiguration was proposed. It was based on the radial basis function network (RBF) which was designed by efficient algorithm of on-line training and parameter optimization. Using multiple model adaptive technique, a set of adaptive neural network observers were designed to restrain modeling uncertainties and the output couple in flight control.
Fault Diagnosis and Fault-Tolerant Control and Guidance for Aerospace demonstrates the attractive potential of recent developments in control for resolving such issues as flight performance, self protection and extended-life structures. Importantly, the text deals with a number of practicallyBrand: Springer-Verlag London.
3. Fault diagnosis and flight envelope assessment Considered the characteristic of control surface damage in flight control systems, a scheme of real- time fault diagnosis and envelop assessment is introduced (illustrated in Fig.1).Cited by: 2.Initial coverage of basic definitions and ideas and a literature review gives way to a treatment of electrical flight control system failures: oscillatory failure, runaway, and jamming.
Advanced fault detection and diagnosis for linear and linear-parameter-varying systems are described.The International Journal of Robust and Nonlinear Control promotes development of analysis and design techniques for uncertain linear and nonlinear systems.
Fault Diagnosis and Fault‐Tolerant Control in Aerospace Systems. Pages: i, 10 November Multiobjective optimization–based fault‐tolerant flight control system.