• 한국정보통신학회논문지
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• 제14권8호
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• pp.1776-1782
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• 2010

간섭형 Fiber optic gyroscope(FOG)는 Sagnac 효과를 이용한 회전센서로 알려져 있으며, 성능 개선을 위한 연구가 수행되어 왔다. 본 논문은 개루프 방식의 FOG 개발과 FPGA를 이용한 디지털 신호처리 기술을 다루고 있다. 첫 번째 목표는 양호한 bias stability(0.22deg/h), Scale factor stability, 단일모드 광섬유를 이용한 낮은 Angle randomwalk(0.07deg/$\sqrt[]{h}$)와 저가의 중급 자이로(Pointing grade)의 설계를 목표로 하고 있다. 두 번째 목표는 광검출기의 출력신호를 고속 ADC로 직접 변환 후 디지털 신호처리를 하는 FOG용 FPGA 개발이다. 본 연구에서 사용한 Cascaded integrator-comb(CIC)타입의 데시메이션 필터는 Adder와 Shift register만으로 구성되어 적은 계산량을 요구하므로 모든 디지털 FOG 프로세서를 저가의 프로세서로도 사용이 가능하다.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2001년도 추계학술대회 논문집 전기물성,응용부문
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• pp.201-204
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• 2001

본 논문에서는 전력케이블, 전력용 변압기 및 가스 절연차단기와 같은 전력설비의 열화로 인한 방전현상 검출을 위해서 간섭계형 광섬유 센서를 제작하고, 방전 현상을 측정하였다. 광섬유 센서는 아크릴과 알류미늄 광섬유를 수회 감은 맨드릴형으로 선택하였으며, 간섭계는 Sagnac 간섭계를 선택하여 실험하였다. 방전현상은 절연유내에 방전모의셀을 설치하여 방전현상을 일으켰고, 광섬유 센서로 방전신호를 검출하였다.

• 한국광학회:학술대회논문집
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• 한국광학회 2009년도 동계학술발표회 논문집
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• pp.303-303
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• 2009

• 항공우주기술
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• 제9권2호
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• pp.31-35
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• 2010

The Ring Laser Gyroscope makes use of the Sagnac effect within a resonant ring cavity of a He-Ne laser and has more accuracy than the other gyros. The space launch vehicle use require the high accuracy Gyro to control and determine the altitude to deliver the satellite in the space. In this paper, The theory of the Path Length Control is explained. The electrical design of Path Length Controller is described. The Design for Path Length Controller is composed of the demodulator, integrator, phase shifter, high voltage amplifier. We apply the circuit to 28cm square ring laser gyro and get the test results.

• Journal of Astronomy and Space Sciences
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• 제23권2호
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• pp.161-166
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• 2006

이 논문에서는 위성 자세제어용으로 사용되는 RLG(Ring Lager Gyroscope) 전류 안정화 회로에 대해서 설명한다. RLG는 헬륨-네온레이저의 공진기 내에서 샤냑효과를 이용한다. 두 방전전류의 차이는 자이로 바이어스 오차의 한 부분을 차지한다. 전류 안정화회로의 이론적 배경과 설계과정에 대해서 기술하고, 입력전압 시험, 온도시험을 통하여 검증하였다.

• 한국군사과학기술학회지
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• 제12권2호
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• pp.222-227
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• 2009

The bias characteristics due to the changes of temperature and temperature gradient of fiber coil are investigated in fiber-optic gyroscope. The bias performance is degraded with the changes of temperature and temperature gradient of fiber coil. The temperature compensation using both the temperature-dependent bias measurement and the temperature-induced error model of fiber-optic gyroscope improves the bias stability about 3 times as much as the uncompensated original case, which leads to very stable bias performance over the temperature range from $-35^{\circ}C$ to $+77^{\circ}C$.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2009년도 정보 및 제어 심포지움 논문집
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• pp.341-343
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• 2009

The Ring Laser Gyroscope makes use of the Sagnac effect within a resonant ring cavity of a He-Ne laser and has more accuracy than the other gyros. The Low Earth Orbit satellite for observatory use require the high accuracy Gyro to control and determine the altitude because of the need of payload pointing accuracy. In this paper, The theory of the Path Length Control is explained. The electrical design of Path Length Controller Is described. The Design for Path Length Controller is composed of the demodulator, integrator, phase shifter, high voltage amplifier. We apply the circuit to 28cm square ring laser gyro and get the test results.

• 전기학회논문지
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• 제57권2호
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• pp.256-260
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• 2008

The Ring Laser Gyro makes use of the Sagnac effect within a resonant ring cavity of A He-Ne laser and has more accuracy than the other Gyros. The Low Earth Orbit satellite for observatory use require the high accuracy Gyro to control and determine the altitude because of the need of payload pointing accuracy. In this paper, The theory of the Path Length Control is explained. The electrical design of Path Length Controller is described. The Design for Path Length Controller is composed of the demodulator, Integrator, Phase shifter, High Voltage Amplifier. We apply the circuit to 28cm square ring laser gyro and get the test results.

• 전기학회논문지
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• 제57권9호
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• pp.1584-1588
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• 2008

The Ring Laser Gyroscope makes use of the Sagnac effect within a resonant ring cavity of a He-Ne laser and has more accuracy than the other gyros. The Low Earth Orbit satellite for observatory use require the high accuracy Gyro to control and determine the altitude because of the need of payload pointing accuracy. In this paper, The theory of the Path Length Control is explained. The electrical design of Path Length Controller is described. The Design for Path Length Controller is composed of the demodulator, integrator, phase shifter, high voltage amplifier. We apply the circuit to 28cm square ring laser gyro and get the test results.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1999년도 하계학술대회 논문집 E
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• pp.2066-2068
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• 1999

In this paper, an optical fiber sensor(OF sensor) utilizing the principal of Sagnac interferometer was proposed to detect the discharge signals which generated from needle-sphere electrode system in insulating oil. The performance of OF sensor was checked by sinusoidal calibration signal generated by PZT acuator at 198kHz. The detected discharge signals consisted of acoustic signal and the electrical noise. The noise signal could be removed by digital low pass filter. It was demonstrated that the OF sensor in this research had a possibility to detect the discharge signals in power apparatus.