• International Journal of Aeronautical and Space Sciences
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• v.8 no.1
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• pp.105-114
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• 2007

This article presents the details of a designed control moment gyroscope (CMG) with a constant speed momentum wheel and one-axis-gimbal, and its experimental results performed at Korea Aerospace Research Institute. The CMG which is able to produce a torque of lOO mNm per each, is mounted in a pyramid configuration with four SGCMGs. Each CMG test and a single axis maneuver test with four-CMG cluster configuration are performed to confirm their performance on a ground-test facilities consisted of three major parts: a vibration isolation system, a dynamic force plate (Kistler sensor), and a DSP board. These facilities provide the accurate data of three axial and torques from the control moment gyro. Details of the CMG experimental results are presented with discussion of the experimental errors. The experimental data are compared with theoretical results and both results are used to verify their performance specifications.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2001.05a
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• pp.115-120
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• 2001

A gyroscope is a rotating body possessing one axis of symmetry and whose rotation about the symmetry axis is relatively large compared with the rotation about any other axis. Tuning fork is this type of structure that various modem gyro-sensors are based on. In this paper, dynamic behavior of a cantilevered beam subjected ta a base rotation with respect to the eccentric axis that is parallel to the beam axis is analyzed. The final equations of motion in terms of generalized coordinates can be solved with numerical scheme with various values of angular velocities and angular accelerations of the rotating axis. In contrast to the case of rotating cantilever beam like helicopter blade, the rotational motion with respect to the beam axis has effect to decrease the stiffness of the beam and has unstable region depending on the magnitude of the rotational angular velocity and angular acceleration.

• Proceedings of the Optical Society of Korea Conference
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• 2000.02a
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• pp.250-251
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• 2000

모드록킹된 광섬유 레이저 자이로스코프(ML-FLaG)$^{(1)}$ 는 일반 거울과 Sagnac 루프 거울로 이루어진 공진기 안에 이득 매질이 포함된 광섬유 레이저의 형태를 가진다. Sagnac 루프 거울을 서로 반대 방향으로 진행하는 두 빛 사이의 위상차를 변조시키면 루프 거울의 반사율이 변조되는데, 여기서 위상 변조 주파수를 공진기의 종모드 간격과 일치시키면 공진기 왕복 주기에 두 개의 펄스가 들어가는 모드록킹된 펄스열을 얻을 수 있다. 이 두 펄스 사이의 시간 간격은 회전율에 따라서 변하기 때문에, 두 펄스 사이의 시간 간격 변화를 측정하면 회전 각속도를 알아낼 수 있다. (중략)

• Korean Journal of Optics and Photonics
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• v.12 no.1
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• pp.10-16
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• 2001

A new digital serrodyne (DS) signal processor for the close-loop fiber optic gyroscope was designed and implemented. It is based on a new algorithm that can solve the remaining problems of the existing digital serrodyne processing by utilizing a new modulation wavefonn. The algorithm was implemented in an FPGA and tested. Theoretical limit and experimental value of the random walk were measured to be 2.6 and 3.3 deg/hr/$\sqrt{Hz}$, respectively. And drift of the processor is smaller than that by Shupe's effect.effect.

• Proceedings of the Optical Society of Korea Conference
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• 2007.02a
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• pp.215-216
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• 2007

Isolator가 삽입된 Erbium 첨가 광섬유광원을 제작하였고 그 특성을 측정하였다. Isolator 삽입 유무에 따른 광섬유광원의 전 온도구간($-32^{\sim}75^{\circ}C$)에서의 중심파장 안정도는 수 ppm으로 큰 차이를 보이지 않았고, 귀환광 변화($-22^{\sim}-20dB$)에 따른 중심파장 안정도에서는 isolator 삽입이후에 1.6ppm으로 귀환광 변화에 매우 둔감한 결과를 얻었다.

• Journal of Institute of Control, Robotics and Systems
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• v.20 no.4
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• pp.437-442
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• 2014

Due to electrical cross-coupling between modulation voltage and photodetector output in a closed-loop fiber optic gyro, deadzone inevitably occurs. In this paper, deadzone error by cross-coupling effect was analyzed and the overcoming method was suggested. Simulation and measurement results show the main reason for deadzone is mainly related to electrical cross-coupling, and it can be effectively reduced by square-wave dithering method.

• Proceedings of the KIEE Conference
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• 1997.11a
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• pp.92-94
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• 1997

A stabilizing system of EOTS is constructed. This system has two major parts. One of them is for detecting the moving motion of a vehicle with electronic gyroscope. The other is for driving of two axes of the platform where the sensor is attached. The controller used in this paper is DSP(TMS320c31) and two BLDC DD motor are used.

• The Transactions of The Korean Institute of Electrical Engineers
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• v.57 no.2
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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.

• Proceedings of the KIEE Conference
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• 2008.07a
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• pp.1807-1808
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• 2008

When it is used for autonomous mobile robots by using dead-reckoning system, odometry system with encorder is the simplest method as well as well-known in the industry. However, odometry system is reflected slide, friction and mechanical errors of wheels when operating the position estimation. And also in order to minimize errors of direction angle which is the most important factor that it is designed the controller in controlling kinematics and quadratic curve, PID that came into the values of sensor fusion with encorder and gyroscope sensor. After designing, the autonomous mobile robot is producted practically and inspected how it works.

• Proceedings of the KIEE Conference
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• 2008.07a
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• pp.1486-1487
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• 2008

MEMS 각속도계에서 일정한 크기와 주파수를 가지는 진동을 주기 위한 공진기 회로는 각속도계의 성능에 가장 큰 영향을 미친다. 특히 공진기 회로에서 기계구조물의 미세한 진동에 의해 발생되는 수 pico-coulomb의 전하를 증폭하는 전하증폭기와 feedback된 신호를 안정된 크기로 만들어 주는 AGC(Automatic Gain Control) 회로의 정밀도가 MEMS 각속도계의 정밀도를 결정짓는다. 본 논문에서는 전하증폭기의 실제적인 회로의 등가 회로 출력 공식을 실험을 통하여 확인하였고, 입력 신호의 주파수가 MEMS 각속도계의 설계 공진 주파수인 30kHz일 때 0.15 pC 단위까지 측정 가능함을 확인하였다. AGC회로의 경우 simulation을 통하여 동작을 확인하였고, 실제 AGC 회로를 제작하여 실험한 결과, 오실로스코프로 확인하기 어려울 정도로 안정된 출력을 얻었다.