• Journal of Navigation and Port Research
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• v.28 no.8
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• pp.653-657
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• 2004

The authors aim to design further an upgraded and self-contained position fixing system to meet the future commercial requirements. As a first step this paper is to investigate the theoretical structure of position fixing based on the nature of free gyro, in which the tilt angles of the two spin axes at an arbitrary position are measured respectively and the elapsed time with respect to a reference position or starting point is observed And it illustrates some limitations to be expected in this system.

• Aerospace Engineering and Technology
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• v.6 no.2
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• pp.150-156
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• 2007

In this paper, we focus on the fault detection and isolation(FDI) method for inertial navigation system with three two-degree of freedom dynamically tuned gyros(DTG) on orthogonal sensor configuration. we propose the FDI method which can detect the fault of each DTGs rather than the fault of each sensing axis. The proposed FDI method is separated into two FDI modules according to the fault magnitude in order to improve the reliability of fault detection information. For large fault detection, only instantaneous DTG measurement is used to detect a fault DTG within a short time. For small fault detection, the integrated value of DTG measurements are used to detect a fault DTG. It takes a more time to detect a fault but it serves more reliable fault detection information. Using the proposed FDI method with consideration of DTG fault characteristic, we could find out a fault DTG successfully.

• Journal of Sensor Science and Technology
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• v.10 no.1
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• pp.1-8
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• 2001

Conventional microgyroscopes of vibrating type require resonant frequency tuning of the driving and sensing modes to achieve high sensitivity. These tuning conditions depend on each fabricated microgyroscopes, even though the microgyroscopes are identically designed. A new micromachined resonator, which is applicable to microgyroscopes with self-toning characteristics, is presented. Since the laterally driven two degrees of freedom (2DOF) resonator was designed as a symmetric structure with identical stiffness in two orthogonal axes, the resonator is applicable to vibrating microgyroscopes, which do not need mode tuning. A dynamic model of the resonator was derived considering gyroscopic application. The dynamic model was evaluated by experimental comparison with fabricated resonators. The microgyroscopes were fabricated using a simple 2-mask-process of a single polysilicon layer deposited on an insulator layer. The feasibility of the resonator as a vibrating microgyroscopes with self-tuning capability is discussed. The fabricated resonators of a particular design have process-induced non-uniformities that cause different resonant frequencies. For several resonators, the standard deviations of the driving and sensing frequencies were as high as 1232Hz and 1214Hz, whereas the experimental average detuning frequency was 91.75Hz. The minimum detuned frequency was 68Hz with $0.034mVsec/^{\circ}$ sensitivity. The sensitivity of the microgyroscopes was low due to process-induced non-uniformity; the angular rate bandwidth, however, was wide. This resonator could be successfully applicable to a vibrating microgyroscopes with high sensitivity, if improvements in uniformity of the fabrication process are achieved. Further developments in improved integrated circuits are expected to lower the noise level even more.

• Proceedings of the Korean Society for Agricultural Machinery Conference
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• 2002.07a
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• pp.424-431
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• 2002

마이크로파 주파수는 일반적으로 1㎓-30㎓ 정도로서 주파수가 매우 높기 때문에 도체뿐만 아니라 절연체와 공기 중에서도 전류가 흐르는 성질을 갖는다. 자유공간에서의 마이크로파를 전자파라고도 하며 그 속도는 빛의 속도와 동일하며 자유공간에서 1cm-30cm 파장 범위를 가지므로 센티파라고도 한다. 전자방사(electromagnetic radiation)은 공간을 통하여 시간에 따라 변하는 전자계(electric and magnetic field)에 의한 에너지의 전파(propagation)이며 파동이론과 (wave theory)와 미립자이론(corpuscular theory)에 의해 해석될 수 있다. 전자파 이론(electromagnetic wave theory)의 기초는 1864년 Maxwell이 전자기 현상에 관하여 지배방정식을 수립함으로써 정립되었으며 1888년 Hertz에 의해 마이크로파의 존재가 실험적으로 증명되었다. 이후 마이크로파 기술은 2 차 세계대전을 거치면서 크게 발전하였으며 초기의 레이더 및 통신 등과 같은 군용 기술에서 마이크로파 건조 및 센싱과 같은 산업응용 기술로 발전하게 되었다. 특히 마이크로파 센서기술 및 가열기술은 농업 및 식품분야에 응용되어 마이크로파 응용제품을 선보이게 되었다. (중략)

• Journal of Navigation and Port Research
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• v.37 no.4
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• pp.329-335
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• 2013

This paper is to develop the position error equations including the attitude errors, the errors of nadir and ship's heading, and the errors of ship's position in the free-gyro positioning and directional system. In doing so, the determination of ship's position by two free gyro vectors was discussed and the algorithmic design of the free-gyro positioning and directional system was introduced briefly. Next, the errors of transformation matrices of the gyro and body frames, i.e. attitude errors, were examined and the attitude equations were also derived. The perturbations of the errors of the nadir angle including ship's heading were investigated in each stage from the sensor of rate of motion of the spin axis to the nadir angle obtained. Finally, the perturbation error equations of ship's position used the nadir angles were derived in the form of a linear error model and the concept of FDOP was also suggested by using covariance of position error.

• Journal of Sensor Science and Technology
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• v.8 no.2
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• pp.139-147
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• 1999

In this paper, we present the new angular velocity pick-off method for DTG (dynamically tuned gyroscope) which is widely used in various inertial navigation systems and motion control systems. In case of the external angular velocity input, the proposed scheme can make a smaller tilt-angle rather than that of conventional PI method in the transient and steady state because it has an additional inner rebalance loop with a mathematical model of the real gyroscope. So, without any mechanical redesign of the DTG, its dynamic range can be enlarged by the proposed method. The theoretical analysis and simulation model of DTG with the proposed scheme are given. Finally, the proposed scheme is verified.

• Journal of Aerospace System Engineering
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• v.11 no.1
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• pp.41-46
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• 2017

A new test bench for small multi-rotor type drones has been developed. Six degrees of freedom (DOF) motion is possible due to a ball bushing, wheels, and rotating plates. An FPGA (field programmable gate array) based controller, that supports realtime parallel processing, is used to measure attitude with an accelerometer and a gyro to adjust motor speed. Several tests were performed to check the operational properties of the test bench and the controller. The results show that this test bench is proper for verifying controllers and the control methods of small multi-rotor drones.

• Journal of Korean Philosophical Society
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• v.126
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• pp.377-401
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• 2013

일반적으로 성리학에서는 개인의 이익보다 도덕적 선택을 우선하라고 요구한다. 그러나 "주역"에서는 결코 이익을 죄악시 하지 않는다. 이 글은 성리학자이면서 역학자인 주자의 이익과 도덕에 대한 입장을 추적하는 연구이다. 주자가 소옹의 결정론적 세계관과 도덕적 자유의지를 강조하는 이천의 관점을 결합함으로써 완성하고자 한 것은 "주역"의 서(筮) 속에서 리(理)를 확인할 수 있다는 것이었다. 점서(占筮)의 결과가 그렇게 나오는 것은 그에 해당하는 이치가 있기 때문이라는 말이다. 그런데 "주역"의 리(理) 즉 역리(易理)란 오랜 경험과 관찰을 통해 확보된 사회적 존재로서 인간의 심리적 행위적 경향성의 총합이다. 그리고 그 구체적인 내용은 바로 상황적 합리성과 타자와의 조화로움이다. 이 리(理)는 우주와 사회의 정해진 질서로서 우리에게 주어진다. 개인은 이 주어진 질서에 따를 수 있는 자유와 함께 따르지 않을 수 있는 자유를 지닌다. 때문에 정해진 질서와 그 속에서의 개인의 자유의지는 양립가능한 것으로 받아들여지고, 그런 의미에서 주자는 약한 결정론자라고 할 수 있다. 성리학은 우주의 질서로부터 부여받은 당위의 법칙에 자발적으로 동의할 것을 요구한다. 그것이 가장 올바른 선택이면서 동시에 자신에게 가장 이로운 선택이기 때문이다. 주자는 상황적 합리성과 타자와의 조화로운 관계에서만이 자신의 진정한 이익을 추구할 수 있다고 생각한다. 타자와의 유기적 관계를 부정하고 유아적(唯我的) 이익만 추구하려는 자는, 사회적 존재로서 인간이 지니는 심리적 행위적 경향성을 무시한 어리석은 자이다. 이렇게 주자에게서 이익[리(利)]은 상황적 합리성[의(宜)]이 되고 또 그것은 바로 도덕[의(義)]이 된다. 참다운 의미에서의 합리적인 판단은 도덕적 선택을 불러온다.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2010.05a
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• pp.725-727
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• 2010

For simulation of Boat motion, pitch, motion element of roll and yaw direction could simulated. The combination of the marine use various multi sensor surveillance system technology with the development of servo motion control algorithm and gyro sensor in six freedom motion is implemented to analyze the movement response. The stabilization of the motion control is developed and Nano driving Precision Pan-Tilt/Gimbal system is obtained from the security positioning cameras with ultra high speed device is used to carry out the exact behavior of the device.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2018.11a
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• pp.328-330
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• 2018

A floating body with a device that converts solar energy into electrical energy is moved by waves. To evaluate the safety of a floating body, measurement and interpretation of the float motion is required, which is generally based on 6 degrees of freedom motion. The 6 degree of freedom motion can be measured using MEMS (Micro-Electro Mechanical System), which features low power, small size and low cost. The key issue is, meanwhile, the low precision of the MEMS. In this study, the safety evaluation technique by analyzing the behavior of floating body using MEMS was examined. As a result of the study, it was found that the marine floating body can be modeled through the inertial measurement platform using the 3-axis accelerometer and the 3-axis gyroscope, and the safety of the float can be evaluated through this model.