• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.5
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• pp.57-64
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• 2005

Modern versions of supersonic jet fighter aircraft using digital flight-by-wire flight control system receive aircraft flight condition such as altitude, airspeed and AoA(angle of attack) from IMFP(Integrated Multi-Function Probe). IMFP sensors data have triplex structure using three IMFP sensors. An air data reconfiguration mode is applied to a T-50 flight control law to guarantee the aircraft flight stability when 2 or 3 IMFP sensors data are invalided. In this study, linear analysis and HQS(Handling Quality Simulator) pilot simulation are performed to analyze flight stability when the air data reconfiguration mode is applied to the control law. And we propose an example that the air data reconfiguration mode is applied to the control law due to second failure of IMFP during T-50 flight. It is found that the aircraft flight stability is not affected when the T-50 flight control law is changed to the air data reconfiguration mode.

• Proceedings of the KIEE Conference
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• 2003.04a
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• pp.72-74
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• 2003

유도전동기의 가변속 구동시스템에서 자속 축 기준제어를 이용하는 경향이 증가하고 있으며 설치환경, 가격 등의 제약으로 인하여 위치 및 속도센서가 없는 센서리스 속도제어가 많이 연구되고 있다. 본 논문은 유도전동기의 센서리스 제어에 관한 연구로서 과도상태에서 슬라이딩모드 관측기를 사용함으로써 속응성이 빠르고 파라미터의 변동에 강인하며, 정상상태에서는 적응상태관측기를 사용함으로써 채터링을 감소하는 센서리스 제어를 제시한다. 시뮬레이션 및 실험결과에서 과도상태와 정상상태에서 양호한 성능을 나타내었다.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2016.10a
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• pp.668-669
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• 2016

The retarder as a hydraulic brake system in order to assist a service brakes in commercial vehicle is operated by automatic and manual mode due to driver. Braking energy by retarder operation is transmitted to the engine radiator of vehicle cooling system, passing through the retarder oil heat exchanger. At this moment, the retarder ECU performs the function that is controlled a braking torque with consideration for automatic and manual mode, temperature of retarder oil/water, engine coolant temperature, vehicle speed, and etc. In this paper, it deals with the design of retarder control logic and the results of retarder braking performance test regarding a cooling system of retarder and vehicle.

• The Transactions of the Korean Institute of Electrical Engineers B
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• v.54 no.1
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• pp.40-46
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• 2005

This paper has investigated the speed sensorless indirect vectorcontrol of a two-phase induction motor to implement adjustable-speed drive for low-power applications. The sliding mode observer estimates rotor speed. The convergence of the nonlinear time-varying observer along with the asymptotic stability of the controller has been analyzed. To define the control action which maintains the motion on the sliding manifold, an "equivalent control" concept is used. It has been simulated and implemented on a sensorless indirect vector drive for 150W two-phase induction motor. The simulation and experimental results demonstrate effectiveness of the estimation method.

• Proceedings of the KIPE Conference
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• 2011.07a
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• pp.208-209
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• 2011

본 논문은 SRM의 센서리스 속도제어를 위한 슬라이딩 모드 자속관측기법을 적용하고, 동일한 센서리스 추정방식으로 초기 기동에서 센서리스 영역까지의 천이 구간에서 오픈루프 속도리플을 억제할 수 있는 방식을 제안한다. 제안된 방식에서 센서리스 위치추정은 슬라이딩으로 자속관측기를 적용하고 있지만, 자속 계산에서 위치오차를 감소하기 위한 오차 성분을 고려하였으며, 특히 초기기동에서 동일한 관측기와 계산된 자속의 오차 성분으로 오픈루프 상태에서의 전류제어를 수행함으로써 천이구간에서의 속도리플을 억제할 수 있다. 제안된 방식은 컴퓨터 시뮬레이션을 통하여 타당성을 검증하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.41 no.2
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• pp.98-106
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• 2013

This paper proposes fault tolerant control laws using sliding mode control and adaptation laws for a satellite with reaction wheel faults. Considering system parameter errors and faults uncertainties in the dynamics of satellite, the control laws were designed. It was assumed that only reaction wheel failures occurred as faults. The reaction wheel faults were reflected in the multiply form. Because the proposed control laws satisfy the Lyapunov stability theorem, the stability is guaranteed. Through computer simulation, it was assured that the proposed adaptive sliding mode controller has a better performance than the existing sliding mode controller under unstable angular rates.

• Proceedings of the Korean Society Of Semiconductor Equipment Technology
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• 2006.10a
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• pp.145-149
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• 2006

반도체의 고집적화와 LCD의 대형화로 인해 웨이퍼 및 LCD 검사용 스테이지의 성능 향상이 요구된다. 본 논문에서는 고속의 검사속도, 서브마이크론의 검사 정밀도, 그리고 대행정 구동을 위한 이중 서보 시스템을 제안하였다. 이중 서보 시스템은 선형모터로 구동되고 공기베어링으로 가이드 되는 조동 구동부와 보이스 코일 모터(VCM)로 구동되고 공기베어링으로 가이드 되는 미세 구동부로 구성된다. 검사 효율을 향상시키기 위한 고속 세틀링을 위한 제어기로서 시간 최적 제어 기법과 시간 지연 제어기를 결합한 모드 변경 제어기를 제안하고 이중 서보 시스템에 구현하여 성능을 평가하였다.

• Proceedings of the KIPE Conference
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• 2017.07a
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• pp.286-287
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• 2017

본 논문은 철도 차량 구동용 IPMSM 제어를 위한 속도 영역별 PWM 알고리즘을 제안한다. 철도 차량의 고속영역 제어는 인버터 전압 이용률을 최대화 할 수 있는 1-Pulse 제어 기법이 요구된다. 그러나, SPWM을 이용한 비동기 1-Pulse 제어는 출력 전류의 불균형을 초래한다. 따라서, 고속영역 제어를 위해 동기화 시킨 후 SPWM을 이용한 1-pluse 제어는 필수적이다. 본 논문에서는 비동기 모드로 제어를 시작하여 과변조 영역 이전에 지령 전압과 삼각파 주파수를 동기화 시킨 후 고속 영역운전을 하는 PWM 알고리즘을 제안한다. 본 논문에서 제안하는 알고리즘은 시뮬레이션으로 검증한다.

• Journal of the Korean Society for Nondestructive Testing
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• v.25 no.1
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• pp.20-26
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• 2005

Ultrasonic guided waves have been widely employed for long range inspection of structures such as plates, rods and pipes. There are numerous modes with different wave velocities, and the appropriate mode selection is one of key techniques in the application of guided waves. In the present work, phase tuning by an array transducer was applied to generate ultrasonic guided waves. For this purpose, 8-channel ultrasonic pulser/receiver and their controller which enables sequential activation of each channels with given time delay were developed. Eight transducers were fabricated in order to generate guided waves by using an array transducer. The selective tuning of wave mode can be achieved by changing the interval between elements of an array transducer.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.42 no.4
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• pp.864-870
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• 2017

This paper describes a Dual Buck Converter with mode control using variable Frequency to Voltage for portable devices requiring wide load current. The inherent problems of PLL compensation and efficiency degradation in light load current that the conventional hysteretic buck converter has faced have been resolved by using the proposed Dual buck converter which include improved PFM Mode not to require compensation. The proposed mode controller can also improve the difficulty of detecting the load change of the mode controller, which is the main circuit of the conventional dual mode buck converter, and the slow mode switching speed. the proposed mode controller has mode switching time of at least 1.5us. The proposed DC-DC buck converter was implemented by using $0.18{\mu}m$ CMOS process and die size was $1.38mm{\times}1.37mm$. The post simulation results with inductor and capacitor including parasitic elements showed that the proposed circuit received the input of 2.7~3.3V and generated output of 1.2V with the output ripple voltage had the PFM mode of 65mV and 16mV at the fixed switching frequency of 2MHz in hysteretic mode under load currents of 1~500mA. The maximum efficiency of the proposed dual-mode buck converter is 95% at 80mA and is more than 85% efficient under load currents of 1~500mA.