• Proceedings of the Korean Institute of Industrial Safety Conference
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• 2002.05a
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• pp.413-418
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• 2002

베어링은 산업현장에서 널리 쓰여지는 중요 부품이다. 따라서 이의 결함에 따른 손실을 예방하기 위해서는 이상을 진단하고 검지하는 기법이 요구된다. 따라서 본 연구에서는 저속회전하므로 노이즈가 많이 포함되어 절상상태의 신호검출이 어려운 저속회전베어링의 외륜이상을 웨이브렛의 Denoising 기법을 적용하여 정량적으로 진단하고 패턴인식법 중의 하나인 KDI(Kullback Discrimination Information)를 적용하여 이상상태의 진단/검지능력을 시험해 보았다. 웨이브랫의 Denoising 기법은 노이즈 캔셀링(Noise canceling)이 능력이 뛰어났고, HDI기법은 저속회전베어링의 정상과 이상의 분류에 뛰어난 검지능력이 있음을 알 수 있었다.(중략)

• Proceedings of the KIPE Conference
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• 2016.07a
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• pp.119-120
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• 2016

회전자 자속기준 벡터제어(FOC)의 센서리스의 기법은 다양하지만, 크게 역기전력을 이용하는 방식과 인덕턴스를 기반으로 하는 방식으로 나눌 수 있다. 역기전력을 기반으로 하는 기법은 중속이상의 영역에서는 뛰어난 성능을 보이지만, 저속영역에서 역기전력이 작기 때문에 저속에서 불리함이 있다. 반면, 인덕턴스를 기반으로 하는 기법 중 캐리어 신호를 주입하는 기법은 전동기의 자기적 돌극성(Magnetic saliency)을 이용하므로 저속에서도 사용가능하지만, 고속에서는 전압제한으로 인하여 전압주입에 불리함이 있으며, 고주파잡음의 문제가 있다. 따라서 본 논문은 저속영역에서 사각파 형태의 고주파 주입 센서리스기법을 사용하고, 중속이상의 영역에서 역기전력 센서리스기법으로 절환(Crossover)하는 방식을 제안한다. 기존의 속도추정 기법과 제안하는 기법을 시뮬레이션을 통해 비교한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.9
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• pp.752-759
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• 2018

This paper presents methods and results of nonlinear simulations for a guided munition for verifying stability at slow spin. The munition is launched by an artillery and it deploys the rear fins to reduce its spin. While the spin speed command is set to 1 rps and 3 rps, wind gusts of 3m/s, 7m/s, 10m/s, and 15m/s in amplitude, and 26 different directions were generated as disturbance for each simulation run. Whereas the munition with the spin speed of 3 rps didn't flip, that with 1-rps spin flipped under some gusts. However, the gusts which increase airspeed in the flight direction didn't introduce harmful effect. Most importantly, all the flips of the munition was observed near the end of the simulation where the munition is going down. No problem was observed near the summit of trajectory.

• Journal of the Korean Institute of Telematics and Electronics T
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• v.35T no.1
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• pp.90-98
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• 1998

This paper is to describe the improved vector control which can control the induction motor robustly in low speed. When the induction motor is drived with low speed, below 10 percent of the rated speed, an algorithm which can compensate the error of unit vector angle generated by the harmonics is proposed. Another algorithm which can be tuned to the rotor time constant so that nay be robust to the rotor parameter change in low speed and transient state was proposed. The ripple of flux and torque was reduced by the proposed vector control and then the stable output characteristics was obtained in low speed. When the input and output is sinusoidal, the proposed vector control, the direct vector control and the indirect vector control were analyzed and compared in the low speed characteristics. And each control characteristics is compared and analyzed in state of containing harmonics. The estimation and tunning performance of rotor time constant is confirmed with simulation. The whole control system is implemented by real hardware and experimented to compare the proposed vector control with the direct vector control. As a result of the experiment with two control methods in low speed, the torque ripple of the proposed vector control is improved by 45 percent than the direct vector control. And it is confirmed that the flux current ripple is reduced in 0.2 p.u. and torque current ripple is reduced in 0.6 p.u. It is confirmed that the rotor time constant by the estimation and the tunning algorithm is tunned by the real rotor time constant. Finally, it was confirmed that the validity and robustness for the proposed vector control in low speed existed.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.9
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• pp.681-689
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• 2020

This paper presents methods and results of both flight test examining roll angle estimation performance of slowly rolling munition forced to spin in the air, and fabricating a replica of guided munition. Guided munition was deployed from multi rotor type UAV mother ship whose altitude and velocity was conveyed to it as initial state. Flight test scenario is composed of a sequence of munition drop(deployment), munition spin, roll angle estimation and stabilization. Munition was deployed from mother ship at around 200m high with horizontal velocity of 15m/s, and was made spun using internal reaction wheel. Performance analysis on roll angle estimation is provided in comparison with commercial aerospace graded GPS/INS. Moreover, several mechanisms that rotates munition using reaction wheel, and actual product that realizes one of them are introduced.

• Proceedings of the KIPE Conference
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• 2017.11a
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• pp.67-69
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• 2017

본 논문에서는 철도차량용 매입형 영구자석 동기전동기의 저속영역에서 구동을 위해 센서리스 제어 기법을 적용하였다. 저속영역에서 센서리스 제어는 회전하는 전동기에 연속적인 고주파 신호를 인가하고 그 신호에 대한 응답을 이용한다. 매입형 영구자석 동기전동기의 회전자 인덕턴스 변화와 자기적 돌극성을 이용하므로 특정 전동기에 대해 우수한 성능을 나타낸다. 따라서 본 논문에서는 동기좌표계 d축 전압에 정현파 신호와 구형파 신호를 주입하여 두 방식에 대한 결과를 시뮬레이션을 통해 분석하였다.

• Proceedings of the KIPE Conference
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• 2017.07a
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• pp.72-73
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• 2017

자동차 라디에이터용 팬과 에어컨 실외기 팬의 경우 영구자석동기 전동기는 자연 상태에서 외부 바람에 의해 임의의 방향과 임의의 속도로 회전할 수 있다. 이런 응용분야에서 회전자 위치검출 센서가 부착되어 있는 경우에는 회전방향 및 속도를 비교적 간단하게 제어할 수 있다. 그러나 회전자 위치검출 센서를 사용하지 않는 센서리스 제어의 경우 외부부하에 의해 회전자가 회전중일 때는 회전자의 위치정보가 없기 때문에 추가적인 알고리즘이 필요하다. 본 논문에서는 외부부하에 의해 회전자가 임의의 방향 및 임의의 속도로 회전하고 있는 경우 원하는 회전방향으로 원하는 속도로 제어하기 위한 센서리스 제어 알고리즘을 제안한다. 회전자가 역방향 및 정방향 저속으로 회전중인 경우와 정방향 고속으로 회전중인 경우에 대해 회전자를 정방향의 주어진 속도로 제어하기 위한 회전자 위치검출 및 센서리스 제어 알고리즘을 제안하고 실험으로 검증한다.

• Journal of Sensor Science and Technology
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• v.6 no.4
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• pp.280-289
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• 1997

The measure of motor speed using encoder is difficult to detect accurate speed and direction in very low speed because the intervals between an encoder pulse and pulse are long. So various speed estimation techniques were proposed to have the good dynamic performance in low speed. And direction detection is so important as speed measurement in very low speed. But because the conventional direction detection circuit check the direction only 1 time in 1 period of each encoder pulses, so it has long delayed detection time in very low speed, thus accurate detection of direction is difficult. In this paper, we propose a 2 way edge detection method which can detect at the rising and filling edge of each encoder pulses. So it can check the direction 4 times in 1 period of each encoder pulses. Therefore if we use proposed method, we can reduce the detection time as 1/4 than that of conventional circuit and can detect more accurate speed and direction. And computer simulation and experiment is performed to verify the perfomance and effect of proposed circuit and we analyze it's results by comparing with that of conventional circuit.

• Journal of the Institute of Electronics Engineers of Korea TE
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• v.39 no.1
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• pp.71-76
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• 2002

Because the driving time is increased under the low speed by rapidly increasing of vehicles, this paper is presented a new ignition control system for improvement the fuel economy, which only some of cylinders are using under the idle status or low speed and preserving the engine rpm. is applicable to effective in fuel economy. An actual hardware was made to prove this new control system. The developed variable cylinder engine concentrated the heat neat the cylinders in idle status or low speed, so there was a problem in re-ignition. It was the reason of a lot of exhaust gas, high fuel consumption and instability of engine revolution. In this paper, in order to solve above problem to show the improvement fuel economy using the new ignition control system and valve opening period at idle status of low speed.

• Proceedings of the KIEE Conference
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• 2002.04a
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• pp.103-105
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• 2002

본 연구에서는 홀소자를 이용한 저가형 엔코더와 제어기를 제안하고 이를 통한 연속적인 회전자 위치추정을 통해 최적의 스위칭 온/오프시점을 결정함으로서 저속 전기자동차 구동용 SRM의 기동특성과 주행성능을 실험을 통해 확인하였다.