• Proceedings of the Korean Society of Fisheries Technology Conference
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• 2000.10a
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• pp.27-28
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• 2000

일반적으로 과학어군탐지기는 임의의 수층에서 어군에 의해 산란된 신호로부터 자원량 추정을 실시한다. 따라서, 대상 어군을 구성하는 개체어의 표적강도(Target Strength ; TS)는 가장 중요한 변수이며, 이로부터 현장에서 어군의 분포 밀도를 좀더 정확하게 추정할 수 있다. TS를 결정하는 변수는 자세각, 어체의 체장, 부레의 유무, 주파수 등이다. TS를 알기 위한 많은 국내ㆍ외의 실험들이 죽은 어체를 이용하였으며, 살아있는 어체라도 음축으로부터 어체의 위치를 정확히 파악하기 어려운 센서들을 사용하여 정확한 TS의 정보를 제공하는데는 한계가 있었다. (중략)

• Journal of the Korean Society of Radiology
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• v.5 no.4
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• pp.179-187
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• 2011

This study statistically analyzed the difference of the stability of maintaining a respiratory period shown according to position and use of a device to search the tendency and usefulness of a device. The supine position showed better maintaining respiratory cycles than the prone position. The 85% of subjects who showed bad maintenance pattern of a respiratory cycle were significantly different pattern with using belly board. It could be said that there was a significant correlation between the maintenance of a respiratory cycle and relative index of respirational stability(p=0.044, kappa=0.607). The movement due to respiration was one of important considerations in the radiation therapy on chest, abdomen, and even pelvis. This study could contribute to the high quality radiation therapy by statistic analysis of respiratory signals and its application.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.40 no.12
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• pp.997-1003
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• 2016

This paper presents an application of adaptive algorithms for yaw moment distribution with electronic stability control (ESC) and active rear steering (ARS) in integrated chassis control (ICC). Integrated chassis control consists of upper- and lower-level controllers. In the upper-level controller, the control yaw moment is computed with sliding mode control required to stabilize a vehicle. In the lower-level controller, adaptive algorithms are applied to determine the required brake pressure of ESC and the necessary steering angle of ARS, in order to generate the control yaw moment. Simulation is performed using the vehicle simulation package CarSim to validate the proposed method.

• Proceedings of the Korean Society of Computer Information Conference
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• 2015.01a
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• pp.183-184
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• 2015

본 논문에서는 HTML5 기반의 대화형 스키점프 시각화 도구를 소개한다. 스키점프의 비거리는 다양한 요소에 영향을 받지만 받음각에 따른 양력과 항력의 비인 양항비에 의해 크게 결정된다. 본 논문에서는 스키의 벌림각, 구부린 각 등을 면적 계수로 두고 물리적인 2차원 좌표를 계산하여 시각화한다. 사용자의 상호작용성을 위하여 각 계수나 영향 요소를 조정할 수 있게 하여 실시간으로 스키점퍼의 자세와 비거리를 확인할 수 있게 하였다. 또한 구현 결과는 웹기반에서 동작하여 사용자의 접근성과 모델 변경에 따른 용이성을 제공한다. 본 논문의 결과물은 스키점프 경기력 향상을 위한 분석 도구로 활용될 수 있을 것이다.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.166.1-166.1
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• 2012

최근에는 정지궤도위성에도 지구센서 대신 별추적기를 탑재하는 추세이다. 별추적기의 경우 태양이나 지구와 같은 밝은 물체가 시야각에 들어올 경우 자세결정을 수행할 수 없기 때문에 별추적기 최적 배치를 위한 해석이 요구된다. 그런데, 정지궤도위성의 경우 24시간을 주기로 태양이 적도면을 회전하고 또한 동지와 하지를 최대로 하여 적도면과 23.5도의 기울기를 갖고 있기 때문에 별추적기 배치에 많은 제한이 발생한다. 별추적기 성능을 최적으로 얻기 위해서는 탑재되는 광학계가 서로 직각이 되어야 하지만 태양 위치에 따른 제한으로 인해 직각이 될 수 없으며 이 경우 성능은 약간의 손실을 감수하면서 항상 태양을 회피하기 위한 최적 각을 적용하거나 태양이 들어올 경우만 성능 손실을 감수하면서 이외의 경우에 별추적기 최적의 성능을 얻고자 하는 방법이 있을 수 있다. 본 연구에서는 이러한 방법들에 대한 해석을 수행하여 최적 각을 소개하였고, 다중머리 별추적기를 대상으로 해석을 수행하였다. 다중머리 별추적기는 하나의 전장품에 광학계가 여러 개 장착되는 제품으로 최근에 우주이력(heritage)를 갖기 시작하였다.

• Journal of the Korean Society of Marine Environment & Safety
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• v.23 no.5
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• pp.574-584
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• 2017

In this paper, the optimizing path finding control method is studied for a Legged-robot. It's named TITAN-VIII. It has a lot of advantages over the wheeled robot in the ability to walk freely on an irregular ground. However, the moving speed on the ground of the Legged-robot is slower than the Wheeled-robot's. Consequently, the purpose of the method is presented in this paper to minimize its time when it walks to a goal. It find the path, our approach is based on an algorithm which is called Dijkstra's algorithm. In the rest of paper, the various posture of the robot is discussed to keep the robot always in the statically stable. Based on above works, the math formulas are presented to determine the joint angles of the robot. After that an algorithm is designed to find and keep robot on the desired trajectory. Experimental results of the proposed method are demonstrated in the last of paper.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.7
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• pp.71-78
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• 2006

Sun sensors are frequently implemented by satellites for attitude sensing, due to its simple manufacturability and light weight. A modeling of sun sensors has an important effect on the accuracy of satellite attitude determination. This paper addresses a new modeling of a 2-axis miniature fine sun sensor with improved accuracy. Unlike other previous algebraic modeling methods, the newly suggested physical modeling method takes into account the shadowing effect of the slit thickness. It was shown that a newly proposed sun sensor modeling provides a substantial accuracy improvement of 29% compared to the generic algebraic modeling. The proposed sensor modeling was validated using 2-axis fine sun sensors with FOV(Field of View) of ${\pm}60^{\circ}$ mounted on HAUSAT-2 small satellite, currently under development by SSRL(Space System Research Lab.) at Hankuk Aviation University, Korea.

• Journal of Aerospace System Engineering
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• v.16 no.4
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• pp.60-67
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• 2022

An Electro-Optical Tracking System (EOTS) is an electric optical system with EO/IR cameras, laser sensors, and an IMU. The EOTS calculates coordinates of targets, using attitude and acceleration measured by the IMU. In particular for an armed aircraft, the performance of the weapon system depends on how quickly and accurately it acquires the target coordinates. The IMU should be operated after alignment is complete, to meet the coordinate accuracy required by the weapon system so the initial stabilization time of the IMU should be reduced, by quickly measuring the attitude and acceleration. Alignment is the process of determining the initial attitude by resolving the attitude error of the IMU, and the IMU of mission equipment such as an airborne EOTS, uses velocity matching based on the velocity from GPS/INS for aircraft navigation. In this paper, a method is presented to improve the transfer alignment performance of the airborne EOTS, by maneuvering aircraft and the mission equipment. First, the performance factor of the alignment was identified, as a heading error through the velocity matching model and simulation results. Then acceleration maneuvers and attitude changes were necessary, to correct the error. As a result of flight tests applied to an EOTS on a OOO aircraft system, the transfer alignment performance was improved as the duration time was decreased, by more than five times when the aircraft accelerated by more than 0.2g and the EOTS was moving until 6.7deg/s.

• Proceedings of the Korean Society of Broadcast Engineers Conference
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• 2016.06a
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• pp.253-255
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• 2016

본 논문에서는 다중 지역 이진 패턴(Multi-scale Bock LBP, MB-LBP) 특징과 랜덤 포레스트에 기반한 새로운 기법의 머리 방향 분류 기법을 제안한다. 제안 기법에서는 occlusion 과 조명의 변화에 강인한 분류 정확도를 얻기 위해서 랜덤화된 트리를 학습하는 것을 목표로 한다. 우선, 얼굴 이미지로부터 많은 MB-LBP 특징을 추출하고, 얼굴 영상들을 랜덤하게 입력하고 MB-LBP 크기 파라미터와 같은 랜덤 특징과 블록 좌표들을 사용하여 트리를 생성한다. 게다가 각 노드에서 정보 이득을 최대화 하는 트리의 내부 노드를 생성하기 위해서 uniform LBP 의 특성을 고려한 분할 함수를 개발한다. 랜덤화된 트리는 랜덤 포레스트에 포함되어 있으며 마지막 결정단계에서 Maximum-A-Posteriori criterion 으로 최종 결정을 한다. 실험 결과는 제안 기법이 다양한 조명, 자세, 표현, occlusion 상황에서 기존의 방법보다 개선된 성능으로 머리 방향을 분류 할 수 있음을 보여준다.

• Journal of the Korean Society of Marine Environment & Safety
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• v.24 no.5
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• pp.591-596
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• 2018

In Designing a Small Ship, the Design of the Trim for Sailing has a great influence on the Stability of the Ship as well as Resistance. The Center of Gravity of a Ship is mostly determined during Initial Design. This Study confirms the Effect of Trim on changes in Vertical Center of Gravity by Numerical Analysis for a Small Catamaran. The Results were examined in a Model test. However, No Model tests were conducted while varying the changes in Vertical Center of Gravity. Nonetheless, Investigation was completed for the Purpose of presenting Vertical Center of Gravity results according to plans for the Trim during Initial Design of a Small Ship. In order to verify the Results of Numerical Analysis, a Comparison with Experimental results was carried out. Alternation of Trim angle and Resistance performance according to changes in the Center of Gravity were studied.