• 한국측량학회지
• /
• 제40권4호
• /
• pp.359-364
• /
• 2022

원격탐사 영상의 변화탐지는 카메라의 광학적 요인, 계절적 요인, 토지피복 특성에 의해 오류가 발생한다. 본 연구에서는 CycleGAN (Cycle Generative Adversarial Network) 방법을 사용하여 촬영 각도에 따른 영상 내 건물 기울기를 모의 조정하였고, 이렇게 모의한 영상을 변화탐지에 활용하여 탐지 정확도 향상에 기여하도록 하였다. CycleGAN 기반으로 두 개 시기 영상 중 한 시기 영상을 기준으로 건물의 기울기를 다른 한 영상 내 건물에 유사하게 모의하였고 원 영상과 건물 기울기에 대한 오류를 비교 분석하였다. 실험자료로는 서로 다른 시기에 다른 각도로 촬영되었고, 건물이 밀집한 도시지역을 포함한 Kompsat-3A 고해상도 위성영상을 사용하였다. 실험 결과, 영상 내 건물 영역에 대하여 두 영상의 건물에 의한 오탐지 화소 수가 원 영상에서는 12,632개, CycleGAN 기반 모의 영상에서는 1,730개로 약 7배 감소하는 것으로 나타났다. 따라서, 제안 방법이 건물 기울기로 인한 탐지오류를 감소시킬 수 있음을 확인하였다.

• 한국항해학회지
• /
• 제5권2호
• /
• pp.1-39
• /
• 1981

A doppler log is the typical device which can measure the ship's speed over the ground directly, by means of doppler effect of the underwater ultrasonic wave, which involves the error due to the sea bottom inclination, the trim and the incorrect transducer installation etc. The present doppler log adopts a single transducer, faced in the direction of themain beam, and therefore it is unable to correct the beam direction to eliminate the above mentioned error. Moreover, the frequencyis also limitted in a comparatively high range for getting a sharp beam with single transducer, and the speed over the ground can not be detectable at the deep sea, for an instance, over 200 meters. This paper describes a theoretical consideration for the doppler log error and an analysis by a computer on the observed speed data by a full size model ship. The result is verified that the most of doppler log error is caused by the ultrasonic beam angle of transducer. To eliminate the doppler log error due to the incorrect transducer installation and also to sharpen the beam for lower frequency range to expand measurable sea depth, this paper proposes a method of controlling the directivity adopting a linear transducer array and of controlling the directivity by the control of exciting current, and investigates by the computer simulation and make experiment with magnetostrictive ferrite transducer of 28, 50 and 75KHz. The experimental results are shown well coincide with the measured ones, and they are revealed that in case where the transducer interval is greater than 1 wavelength, the effective control of the beam direction is hardly performed with keeping adequate beam width and side lobe level. It is concluded that 6-elements array with inter element space of a half wavelength can make comparatively sharp beam and low side lobe level. The results obtained here will contribute very much to the improvement of the performance of doppler log.

• Journal of Astronomy and Space Sciences
• /
• 제12권2호
• /
• pp.265-274
• /
• 1995

The purpose of perigee kick motor firing is to place a satellite into transfer orbit and that of apogee kick motor firing is to place the satellite into geosynchonous orbit in order to increase the semi-major axis of the transfer orbit and reduce the inclination of the transfer orbit. Because apogee motor firing is always accompanied with injection errors, the satellite is not placed into geosynchonous orbit but into a near-geosynchonous orbit, also knows as a drift orbit. Thus, the orbital maneuver to correct drift orbit into gteosynchonous orbit is required, this maneuver is called the station acquisition. For reduction of expenditure and performance of mission, we estimate $\Delta$V budget and required fuel allowance for station acquisition. As the uncertainty of drift orbit by injection error of perigee and apogee kick motor firing prevents us from obtaining exact $\Delta$V budget, statistical Monte Carlo simulation technique is used in order to get optimal $\Delta$V budget and required fuel allowance with a probability of 99%. With respect to Korea satellite launched by Delta-2 launch vehicle in 1995, Monte Carlo analysis is used in order to get various orbital parameters, $\Delta$V budget and required fuel allowance for station acquisition with a probability of 99%.

• 한국정밀공학회지
• /
• 제16권10호
• /
• pp.80-86
• /
• 1999

Since the quality of the coated wires is in various applications dependant on the coating depth, accuracy of hole size of dies used for coating wires must be maintained precisely, in general within one micron. This paper proposes a new vision system which measures automatically the size and shape of small holes having diameters less than 1mm within an error limit of 1 micron. To quickly obtain the focused image, this paper proposes an estimation method of the camera position using only a couple of defocused hole images. It measures the distributions of light intensity around the image boundary and decides the direction and distance of a camera motion. The proposed system measures the size, shape distortion, inclination of the hole against the axis of the dies structure, to decides the acceptability of the dies for use. The proposed algorithm has been implemented using a cheap 640${\times}$480 image system and has shown an average size error of 1micron when measuring the dieses having 0.1mm to 1.0mm diameters. It can be applied to the inspection of the size and position of holes in PCB, too.

• 한국전자파학회논문지
• /
• 제13권1호
• /
• pp.47-52
• /
• 2002

1993년도 ISO에서 \"Guide to Expression of Uncertainty in Measurement\"를 발표함으로써 측정과학에 있어 측정결과의 오차분석 방법을 폐기하기로 사실상 선언하였다. 그리하여 측정의 소급성과 신뢰성을 확보한다는 전제 하에 오차의 개념을 버리고 측정시의 측정불확도를 분석하는 것이 측정과학에 있어서 세계적인 추세이다. 본 논문에서는 전달표준인 열 전압변환기를 사용하여 고주파전압계의 정밀 교정에서 불확도를 산출하기 위하여 수학적 모델을 설정하고 측정에 관계되는 모든 불확도 요인을 분석하였다. 케이블의 영향과 열전대감지기와 직류전압계의 상관관계, 직류소스, RF소스, 감쇠기, 반사계수와 DUT 등 측정에 있어서 관계되는 모든 불확도요인을 분석하여 확장불확도를 산출하였다.확도를 산출하였다.

• 한국정밀공학회지
• /
• 제27권4호
• /
• pp.40-45
• /
• 2010

Evaluation of uncertainty is an ongoing process that can consume time and resources. It can also require the service of someone who is familiar with data analysis techniques. Therefore, it is important for laboratory personnel who are approaching uncertainty analysis for the first time to be aware of the resources required. International inclination of measurement filed to guarantee the traceability and confidence of measurement results discards the error concept and instead analyzes the measurement uncertainty. In this paper, we analyzed the elements of measurement uncertainty on surface roughness test which are the important things in mechanical parts test. Repeat the test by 3 men, the measurement uncertainty could be calculated.

• 한국정밀공학회지
• /
• 제18권11호
• /
• pp.42-50
• /
• 2001

In this paper, a new technique and theory are proposed which correct the orientation (inclination of a vertical axis) of a cylinder in vertical-micro positioning device. An algorithm for determining the orientation of the cylinder with a pair of displacement sensor units is derived and two types of the correction methods are described. To assess the performance and efficiency of the developed correction technique, the compensation errors originated from the correction algorithm and the machined characteristics of cylinder surface are evaluated from the geometrical considerations and the statistical techniques. Based upon the evaluation results, the maximum compensation error is estimated for the orientation of cylinder and the optimum correction technique is derived.

• 한국가시화정보학회지
• /
• 제17권2호
• /
• pp.83-89
• /
• 2019

In this study, we show the maximum cavity radius prediction model that a droplet impacts an inclined bath. Surface tensions, viscosities, inclination angles of a bottom substrate, droplet diameters, falling heights of the droplet are varied for the experiment. We experimentally observe that the cavity grows in hemispherical shape like the cavity formed in a deep bath although the depth of the bath is non-uniform due to an inclined bottom substrate. We derive two theoretical models to predict the experimental results of the fully developed cavity. Although each model has error, we observe that qualitatively theoretical model predicts the trend of experiment results well.

• Journal of Astronomy and Space Sciences
• /
• 제12권1호
• /
• pp.112-122
• /
• 1995

1995년 7월에 발사될 무궁화호 통신위성이 원지점 모터 분사의 오차로 인해 예정된 지구정지궤도진입에 실패했을 경우를 가정하였다. 원지점 모터 분사시에 연료 저장 상태의 불균형, 추력축의 회전 등으로 인하여 원지점 모터 분사가 잘못되어, 통신위생이 정지 궤도 요소 충 궤도 경사각이 $0^{\circ}$가 아닌 지구 통주기 궤도를 도는 상황을 모의실험하였다. 이 때, 궤도 의 진화과정을 섭통론을 통해 분석하였고 이심율과 경사각의 변화를 조사하였다. 궤도 경사각이 $0^{\circ}$가 아닌 지구동주기 궤도를 도는 통신위성이 8자 궤적을 그리게 되면 빔 지향점도 위성의 이동에 따라 움직이는데 이 문제를 해결하기 위해 위성의 roll각을 조정하여 빔 지향점을 고정시킬 수 있는 알고리즘을 무궁화호에 적용시켰다. 그리고 승교정과 강교점을 통과할 때 일어나는 펀파면의 회전 현상도 통신 효율에 큰 영향을 주는데, 편파변의 회전 현상을 줄일 수 있는 yaw각 조정방법올 역시 무궁화호에 적용했다.

• Journal of Positioning, Navigation, and Timing
• /
• 제8권2호
• /
• pp.79-85
• /
• 2019

The mission tasks of polar exploration utilizing unmanned systems such as glacier monitoring, ecosystem research, and inland exploration have been expanded. To facilitate unmanned exploration mission tasks, precise and robust navigation systems are required. However, limitations on the utilization of satellite navigation system are present due to satellite orbital characteristics at the polar region located in a high latitude. The orbital inclination of global positioning system (GPS), which was developed to be utilized in mid-latitude sites, was designed at $55^{\circ}$. This means that as the user is located in higher latitudes, the satellite visibility and vertical precision become worse. In addition, the use of satellite-based wide-area augmentation system (SBAS) is also limited in higher latitude regions than the maximum latitude of signal reception by stationary satellites, which is $70^{\circ}$. This study proposes a local-area augmentation system that additionally utilizes Global Navigation Satellite System (GLONASS) considering satellite navigation system environment in Polar Regions. The orbital inclination of GLONASS is $64.8^{\circ}$, which is suitable in order to ensure satellite visibility in high-latitude regions. In contrast, GLONASS has different system operation elements such as configuration elements of navigation message and update cycle and has a statistically different signal error level around 4 m, which is larger than that of GPS. Thus, such system characteristics must be taken into consideration to ensure data integrity and monitor GLONASS signal fault. This study took GLONASS system characteristics and performance into consideration to improve previously developed fault detection algorithm in the local-area augmentation system based on GPS. In addition, real GNSS observation data were acquired from the receivers installed at the Antarctic King Sejong Station to analyze positioning accuracy and calculate test statistics of the fault monitors. Finally, this study analyzed the satellite visibility of GPS/GLONASS-based local-area augmentation system in Polar Regions and conducted performance evaluations through simulations.