• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.3
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• pp.81-86
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• 2006

This paper deals with a driving current fault monitor design methodology for a DDV actuation system which has a dual hydraulic power supply system, and triplex electric control capability. A fault existing among these redundant channels should be detected accurately and removed timely, and the remaining channels are to be reconfigured in order to compensate the role of a removed faulty channel. An integrated analysis on the aerodynamics, flight control laws, and DDV actuation system is essential for the design of an actuation system fault monitor. A method to define a fault transient boundary which specifies a maximum travel of an actuation system caused by the first faulty operation is proposed based on the top level requirement on the fault effect specified in MIL-F-8785C.

• Proceedings of the KIEE Conference
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• 2011.07a
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• pp.2025-2026
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• 2011

위성의 가장 큰 제한 중에 하나는 발사하면 더 이상의 수리가 불가능하다는 것이다. 그래서 사용하는 위성의 부품 및 시스템에 대하여 신뢰성 검증이 지상에서 많이 이루지고 있지만 모든 고장을 막을 수 있는 것은 불가능함으로 이에 대한 감시 및 고장시 대처하는 기능이 필요하다. 위성의 고장운영(fault management)은 탑재소프트웨어나 하드웨어로 구현하여 운영 중 시스템의 이상상황(anomaly)을 모니터링하고 이상상황이 발생한 경우 시스템이 안전하도록 조치하는 것이다. 본 논문은 천리안위성의 FDIR구조를 소개하였고 탑재체접속장치 경우 설계된 FDIR를 분석하였다.

• Aerospace Engineering and Technology
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• v.6 no.2
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• pp.150-156
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• 2007

In this paper, we focus on the fault detection and isolation(FDI) method for inertial navigation system with three two-degree of freedom dynamically tuned gyros(DTG) on orthogonal sensor configuration. we propose the FDI method which can detect the fault of each DTGs rather than the fault of each sensing axis. The proposed FDI method is separated into two FDI modules according to the fault magnitude in order to improve the reliability of fault detection information. For large fault detection, only instantaneous DTG measurement is used to detect a fault DTG within a short time. For small fault detection, the integrated value of DTG measurements are used to detect a fault DTG. It takes a more time to detect a fault but it serves more reliable fault detection information. Using the proposed FDI method with consideration of DTG fault characteristic, we could find out a fault DTG successfully.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.17 no.7
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• pp.492-498
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• 2016

It is well known that since abrupt faults in induction motors tend to lead to subsequent faults and deterioration of the drive apparatus, motor faults may lead to several operating restrictions, such as security problems and economic loss. A lot of research has been done in the area of diagnosis to detect machine faults and to prevent catastrophic hazards in the motor drive system. This paper presents a new method of motor current signature analysis in which the DC-link current of the inverter-driven induction motor system, where a single current sensor is employed instead of three AC current sensors, is measured, and fast Fourier transform analysis is performed. This proposed method makes it possible to easily discern and clearly separate the motor fault current signature from the normal operation current flowing through the stator and rotor windings.

• Proceedings of the KIPE Conference
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• 2007.07a
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• pp.299-301
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• 2007

본 논문은 무정전 전원공급장치(UPS : Uninterruptible Power Supply System)에서 출력이 중단되는 상황을 최종 출력단에서 감지하여, 첫째 고장 영향의 확산을 차단하고, 둘째 부하에 무정전의 전원공급을 실시할 수 있도록 하는 고속절환장치에 관한 것이다. 본 시스템은 기존 UPS 시스템이 가지고 있는 출력전원을 검출하여 기준전압 범위에서 벗어나면 절체 시키는 일반적인 방식이 아니라, 별도의 시스템을 UPS와는 독립적으로 구성하여 UPS 내부 사고시 고장이 부하와 계통상에도 영향을 주는 현상을 차단하기 위하여 절체 시점에서의 이상적인 접점 상태를 고려하고, UPS의 모든 제어시스템이 불가능한 시점에서도 부하의 연속성을 보장할 수 있도록 구성한 독립제어 고속절환장치 개발에 관한 논문이다.

• Proceedings of the Korean Society of Marine Engineers Conference
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• 2012.06a
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• pp.111-111
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• 2012

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.12
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• pp.1005-1012
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• 2020

Avionics systems that use the PCI-Express bus unfortunately cannot use at least one I/O device if the bus fails, because the I/O device is connected to CPU through only one PCI-Express channel. This paper presents a fault-tolerant architecture of the PCI-Express bus for avionics systems, which tolerates one channel failure with help of the other redundant channel that has not been failed. In this architecture, each redundant PCI-Express channel connects a corresponding port of CPU to each switch logic of channels to provide each I/O device through a switched fault-tolerant channel. This paper includes the results of experimentation to show that the architecture detects the faulty condition in real time and switches the channel to the other redundant channel which has not been failed, when the architecture meets a failure.

• The Journal of the Institute of Internet, Broadcasting and Communication
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• v.16 no.5
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• pp.63-68
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• 2016

Audio mixer is an electronic device which performs a mixing of multiple audio signals. Digital mixer having various functions and scalability is spreaded thanks to advanced DSP and IT technology. However, digital mixer is more vulnerable to stability comparing to conventional analog mixer in the digital error or software error sense because its control is executed by SW. To solve this problem, in this paper, we propose a multi-channel digital analog hybrid mixer scheme, digital mixer error detection mechanism and malfunctioning switching technique. Also we develop the audio mixer having digital-analog hybrid structure. By simulation, we can sense the error of digital mixer except power loss in a 120ms, change into analog mixer mode automatically and provide continuous broadcasting function without mixer function loss.

• Journal of the Korea Institute of Information Security & Cryptology
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• v.29 no.6
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• pp.1403-1412
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• 2019

Effect of damage and loss cost for downtime is huge, if physical devices such as turbines, pipe, and storage tanks are in the abnormal state originated from not only aging, but also cyber attacks on the control and monitoring system like PLC (Programmable Logic Controller). To improve availability and dependability of the physical devices, we design and implement an indirect health monitoring system which sense temperature, acceleration, current, etc. indirectly, and put sensor data into Influx DB in real-time. Then, the actual performance of detecting abnormal state is shown using the indirect health monitoring system. Analyzing data are acquired using the real-time indirect health monitoring system, abnormal state and security threats can be double-monitored and lower maintenance cost utilizing prognostics and health management.

• The Journal of the Korea institute of electronic communication sciences
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• v.11 no.2
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• pp.203-208
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• 2016

This paper presents a fault detection and data processing algorithm for acoustic sensor systems using the multiple sensor algorithm that has originally developed for the wireless sensor nodes. The multiple sensor algorithm can increase the reliability of the sensor systems by utilizing and comparing the measurements of the multiple sensors. In the acoustic sensor system, the equivalent sound level($L_{eq}$) is used to detect the faulty sensor. The experiment was conducted to demonstrate the feasibility of the multiple acoustic sensor algorithm, and the results show that the algorithm can detect the faulty sensor and validate the data.