• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.2
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• pp.144-152
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• 2011

This paper presents a new scheme for fault detection and isolation in the satellite system. The purpose of this paper is to develop a fault detection, isolation and diagnosis algorithm based on the bank of interacting multiple model (IMM) filter for both total and partial faults in a satellite attitude control system (ACS). In this paper, IMM are utilized for detection and diagnosis of anticipated actuator faults in a satellite ACS. Other fault detection, isolation (FDI) schemes using conventional IMM are compared with the proposed FDI scheme. The FDI procedure is developed in two stages. In the first stage, 11 EKFs actuator fault models are designed to detect wherever actuator faults occur. In the second stage of the FDI scheme, two filters are designed to identify the fault type which is either the total or partial fault. An important feature of the proposed FDI scheme can decrease fault isolation time and figure out not only fault detection and isolation but also fault type identification.

• Journal of IKEEE
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• v.23 no.1
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• pp.266-272
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• 2019

Multicopters have become more popular since they are advantageous in their ability to take off and land vertically. In order to guarantee the normal operations of such multicopters, the problem of fault detection and isolation is very important. In this paper, a new method for detecting and isolating an actuator fault of a hexacopter is proposed based on the analytical approach. The residual is newly defined using the angular velocities of actuators estimated by the mathematical model and an actuator fault is detected comparing the residuals to a threshold. And a fault is isolated combining a dynamic model and generated residuals when a fault is detected. The proposed method is a simple, but effective technique because it is based on mathematical model. The results of the computer simulation are also given to demonstrate the validity of the proposed algorithm in case of a single failure.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.38 no.12
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• pp.1177-1183
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• 2010

In this paper, a parallel bank of multiple adaptive unknown input observers approach suggested by D.Wang is applied to detect a single fault of control surface actuator and to estimate the actuator position of lock-in-place fault using a small fixed-wing UAV model with eight control surfaces. This paper shows that not only the fault diagnosis algorithm detects and estimates each faults of lock-in-place in 1 second by simulation but also it may be unavailable to isolate among two same-shaped rudders.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.3
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• pp.67-73
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• 2006

In this paper, a reconfigurable model following flight control method is proposed based on direct adaptive scheme using parameter estimation. Adaptive control scheme updates the control gains to make the system output follow the reference output even when fault occurs. By adopting the frequency domain parameter estimation method, system changes by the fault can be estimated. Recursive Fourier transformation is used for system identification. Using recursive Fourier transform, the proposed adaptive control algorithm guarantees the system stability and improves the system characteristics. To evaluate the performance of proposed control method, numerical simulations are performed.

• Proceedings of the KIEE Conference
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• 2003.07d
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• pp.2094-2096
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• 2003

본 논문에서는 원자력 발전소 제어봉구동장치의 전력변환부에서 발생하는 고장들을 검출하기 위한 새로운 방법을 소개한다. 전력변환부 고장은 제어봉구동장치 동작에 악영향을 미치게 되고 이는 제어봉 오동작으로 이어져 원자로 출력 제어에 차질을 준다. 이러한 이유로 해당 고장의 신속 정확한 검출이 요구된다. 이를 위하여 디지털 시스템 설계용으로 새로운 고장 검출 방법을 도출하고, 기존 웨스팅하우스 모델의 아날로그 맥동 검출기의 약점을 개선하고자 한다.

• Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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• v.23 no.6
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• pp.40-51
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• 2009

To analyze influences under open faults in switching devices of the PWM inverter and under the isolation between the inverter and motor terminal, a faulty model for the inverter-driven permanent magnet synchronous motor is presented. Even though the conventional dq motor model obtained through the transformation of phase voltage model is widely used to analyze and control AC motor, it can not be used under open faults in switching devices since the 3-phase balanced condition is no longer hold under the open fault and it is not easy to obtain motor input voltages in open phase from the pole voltage. To deal with this problem, a faulty model for an inverter-driven permanent magnet synchronous motor is derived by using the line voltage of motor according to switch open, which can be effectively used for performance evaluation of the diagnostic algorithm. The validity of the proposed faulty model is verified through comparative simulations and experiments using DSP TMS320F28335.

• Proceedings of the KIEE Conference
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• 2006.04b
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• pp.74-76
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• 2006

최근 중 저압용 진공 차단기의 구동 메커니즘으로 영구자석형 조작기(PMA)가 널리 사용되고 있다. 이는 모터 스프링이나 유압 및 공압식 등과 같은 기계식 메커니즘에 비해 성능과 신뢰성에서 우수함을 인정받고 있다. 그러나 기존 영구자석형 조작기에서는 가동자와 영구 자석 사이의 큰 마찰력으로 인한 에너지 손실과 차단부와의 연결 로드에서의 기계적 고장 및 파손이 유발될 수 있다. 본 논문에서는 가동자의 로드에 베어링 타입의 부싱을 장착한 모델을 제안함으로써 이 문제를 해결하고자 한다. 부싱을 이용하여 영구 자석과 가동자 사이의 공극을 확보함으로써 마찰을 감소시키고 기계적 안정성 및 동작 특성 향상을 기대할 수 있다. 유한요소법(FEM)과 시간차분법(TDM)을 이용하여 제안된 모델의 동작 특성을 해석하였고, 이를 기존 모델의 특성과 비교하여 그 우수성을 검증한다.