• Title/Summary/Keyword: fault tolerance system

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Design of Self-Repairing Suspension Systems via Variable Structure Control Scheme (가변구조 제어기법을 이용한 고장허용 현가장치 설계)

  • 김도현
    • Journal of Institute of Control, Robotics and Systems
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    • v.8 no.11
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    • pp.922-927
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    • 2002
  • A variable structure control (VSC) based model following control system that possesses fault detection and isolation (FDI) capability as well as fault tolerance property is proposed. The nonlinear part of the proposed control law. whose magnitude is determined by sliding variables, plays the role of suppressing fault effect. Thus, approximate fault reconstruction is also possible via the analysis of sliding variables. The proposed algorithm is applied to an active suspension system of pound vehicles to verify its applicability.

System Reliability (시스템 信賴性)

  • 김동주
    • The Magazine of the IEIE
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    • v.5 no.1
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    • pp.31-37
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    • 1978
  • The value of a system is highly dependent upon its reliability, Reliability means not merely correctness but means fault tolerance of the system. This paper emphasizes software fault tolerance in design stage especially in case of computer controlled system. The general method of fault tolerance design especially including dual computer system and its advantage and disadvantage was introduced. Finally for example of fault tolerance design we would like to present our GTK-500 EPABX.

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State-Monitoring Component-based Fault-tolerance Techniques for OPRoS Framework (상태감시컴포넌트를 사용한 OPRoS 프레임워크의 고장감내 기법)

  • Ahn, Hee-June;Ahn, Sang-Chul
    • Journal of Institute of Control, Robotics and Systems
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    • v.16 no.8
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    • pp.780-785
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    • 2010
  • The OPRoS (Open Platform for Robotic Services) framework is proposed as an application runtime environment for service robot systems. For the successful deployment of the OPRoS framework, fault tolerance support is crucial on top of its basic functionalities of lifecycle, thread and connection management. In the previous work [1] on OPRoS fault tolerance supports, we presented a framework-based fault tolerance architecture. In this paper, we extend the architecture with component-based fault tolerance techniques, which can provide more simplicity and efficiency than the pure framework-based approach. This argument is especially true for fault detection, since most faults and failure can be defined when the system cannot meet the requirement of the application functions. Specifically, the paper applies two widely-used fault detection techniques to the OPRoS framework: 'bridge component' and 'process model' component techniques for fault detection. The application details and performance of the proposed techniques are demonstrated by the same application scenario in [1]. The combination of component-based techniques with the framework-based architecture would improve the reliability of robot systems using the OPRoS framework.

Implementation of IEEE 1451 based Dual CAN Module for Fault Tolerance of In-Vehicle Networking System (차량 네트워크 시스템의 결함 허용을 위한 IEEE 1451 기반 중복 CAN 모듈의 구현)

  • Lee, Jong-Gap;Kim, Man-Ho;Park, Jee-Hun;Lee, Suk;Lee, Kyung-Chang
    • Journal of Institute of Control, Robotics and Systems
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    • v.15 no.7
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    • pp.753-759
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    • 2009
  • As many systems depend on electronics in an intelligent vehicle, concern for fault tolerance is growing rapidly. For example, a car with its braking controlled by electronics and no mechanical linkage from brake pedal to calipers of front tires(brake-by-wire system) should be fault tolerant because a failure can come without any warning and its effect is devastating. In general, fault tolerance is usually designed by placing redundant components that duplicate the functions of the original module. In this way a fault can be isolated, and safe operation is guaranteed by replacing the faulty module with its redundant and normal module within a predefined interval. In order to make in-vehicle network fault tolerant, this paper presents the concept and design methodology of an IEEE 1451 based dual CAN module. In addition, feasibility of the dual CAN network was evaluated by implementing the dual CAN module.

A fault detection and recovery mechanism for the fault-tolerance of a Mini-MAP system (Mini-MAP 시스템의 결함 허용성을 위한 결함 감지 및 복구 기법)

  • Mun, Hong-Ju;Kwon, Wook-Hyun
    • Journal of Institute of Control, Robotics and Systems
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    • v.4 no.2
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    • pp.264-272
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    • 1998
  • This paper proposes a fault detection and recovery mechanism for a fault-tolerant Mini-MAP system, and provides detailed techniques for its implementation. This paper considers the fault-tolerant Mini-MAP system which has dual layer structure from the LLC sublayer down to the physical layer to cope with the faults of those layers. For a good fault detection, a redundant and hierarchical fault supervision architecture is proposed and its implementation technique for a stable detection operation is provided. Information for the fault location is provided from data reported with a fault detection and obtained by an additional network diagnosis. The faults are recovered by the stand-by sparing method applied for a dual network composed of two equivalent networks. A network switch mechanism is proposed to achieve a reliable and stable network function. A fault-tolerant Mini-MAP system is implemented by applying the proposed fault detection and recovery mechanism.

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HM System Design for Fault Tolerance on the IMA System (IMA 시스템에서의 Fault Tolerance를 위한 HM 시스템 설계)

  • Ko, Young-Kwan;Lee, Seung-Hoon;Park, Se-Young;Ban, Chang-Bong;Kang, Dai-Il;Jeong, Jae-Yeop;Lee, Cheol-Hoon
    • The Journal of the Korea Contents Association
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    • v.12 no.8
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    • pp.77-86
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    • 2012
  • Avionics system are composed of multiple electronic device that performs important missions the number of electronic devices for the performance of aircraft has been gradually increasing. As a result, cost of development, maintenance and operating have increased. To solve this problem, technology paradigm of avionics has been shifting from federated avionics systems that manage to each system independently to IMA(Integrated Modular Avionics) systems. Unlike federated systems, fault tolerance becomes an essential technology in IMA systems. Because each aircraft features integrated in the an IMA system, a fault can jeopardize the entire system. In this paper, we define faults which can occur on the ARINC 653 based IMA system first, and design the ARINC 653 compliant HM(health Monitoring) system for the system can continue to operate be normal when occur a fault.

A study on Hardware Redundancy Architecture of Fault-Tolerant System (결함허용 시스템의 하드웨어 여분구조에 대한 연구)

  • shin Ducko;Lee Jong-woo;Lee Jae-ho;Lee Key-seo
    • Proceedings of the KSR Conference
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    • 2003.05a
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    • pp.450-455
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    • 2003
  • This paper is to discuss the hardware redundancy architecture of fault-tolerance system with using redundancy. Each architecture will be studied to implement fault-tolerance in classifying hardware redundancy architecture as passive, active and hybrid hardware redundancy. Therefore Fault-Masking and Fault-Detecting Techniques in each redundancy architecture is studied.

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A New Artificial Immune System Based on the Principle of Antibody Diversity And Antigen Presenting Cell (Antibody Diversity 원리와 Antigen Presenting Cell을 구현한 새로운 인공 면역 시스템)

  • 이상형;김은태;박민용
    • Journal of the Institute of Electronics Engineers of Korea CI
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    • v.41 no.4
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    • pp.51-58
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    • 2004
  • This paper proposes a new artificial immune approach to on-line hardware test which is the most indispensable technique for fault tolerant hardware. A novel algorithm of generating tolerance conditions is suggested based on the principle of the antibody diversity. Tolerance conditions in artificial immune system correspond to the antibody in biological immune system. In addition, antigen presenting cell (APC) is realized by Quine-McCluskey method in this algorithm and tolerance conditions are generated through GA (Genetic Algorithm). The suggested method is applied to the on-line monitoring of a typical FSM (a decade counter) and its effectiveness is demonstrated by the computer simulation.

A Study on Fault-Tolerance Design Methods for Nuclear Digital Control Systems (원전 디지털 제어계통을 위한 고장허용설계방법론에 관한 연구)

  • Go, Won-Seok;Choe, Jung-In
    • The Transactions of the Korean Institute of Electrical Engineers D
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    • v.49 no.1
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    • pp.1-9
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    • 2000
  • In this paper, a design method of fault-tolerance is presented for the nuclear digital control systems composed of software and hardware. As a quantitative design method measure of fault-tolerance, we used Reliability, Availability and Safety. To implement the proposed fault-tolerance, a prototype system has been devised for the digital control systems and a quantitative method of 'Markovian Model' is applied. The results provide the appropriate degree of redundancy and diversity, and fail-safe.

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On Fault Handling in Control Systems

  • Staroswiecki, Marcel
    • International Journal of Control, Automation, and Systems
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    • v.6 no.3
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    • pp.296-305
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    • 2008
  • Whereas fault diagnosis has been the subject of intensive research since the 1970s, the design of fault tolerant systems is a recent research field which does not set its foundations in a unified framework and does not use a unified vocabulary. As a contribution to this special issue, this paper proposes an ontology for the problem of Fault Handling, that embeds the problem of Fault Tolerance.