• The Bulletin of The Korean Astronomical Society
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• v.36 no.2
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• pp.129.2-129.2
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• 2011

망원경을 사용하여 천체를 관측할 때, 망원경은 기계적인 오차, 구동제어 오차 등의 영향을 받는다. 제어를 위하여 천체영상을 획득하는 부분은 시간 지연, 상의 왜곡 등의 영향을 받는다. 더우기, 바람이나 진동 등 예기치 않은 외부적인 요인에 의한 오차가 유발되기도 한다. 이러한 다양한 요인들은 망원경이 천체를 정확히 찾아가고 추적하는 것을 어렵게 만든다. 우리는 추적오차에 주는 영향들을 정량적으로 분석하고 제어에 반영하여 가장 최적의 제어를 할 수 있도록 하고자 한다. 이전 연구에서 김해천문대 독일식 적도의 방식 200mm 망원경과 PLC 기반의 망원경 제어 장치 및 AP8 CCD 카메라를 사용하여, 지향 및 추적 관측 실험을 하였고, 그 결과를 분석하여 경험적 제어 모형을 만들었다(강용우 외, 2010). 이전 연구를 기반으로 이번 연구에서는 제어 전달을 해석적 함수로 시스템의 수학적 모델을 세워, 각 요인들의 영향을 분석하여, 그 내용을 소개하고자 한다.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• v.2
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• pp.435-438
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• 2006

위성신호는 저앙각에 위치하거나 재밍 및 간섭신호의 영향을 받으면 약해진다. 이러한 약신호를 안정적으로 추적하기 위해서는 신호추적루프의 대역폭이 가능하면 작아야 한다. 그러나 작은 대역폭의 신호추적루프는 고기동 환경에서 기준주파수의 주파수오차를 포함한 입력오차가 커져 불안정해진다. 본 논문에서는 최대 저크 15g/s의 동적특성을 가지는 항체의 항법정보를 획득하고 동시에 28dB-Hz의 약신호도 안정적으로 추적할 수 있는 신호추적루프를 연구한다. 이를 위해 위성신호 상태를 예측할 수 있는 SNR, 앙각, 항체의 가속도 등을 고려하여 대역폭 및 PIT를 가변적으로 설계한 적응형 신호추적루프를 설계한다. 또한 약신호인 C/No 28dB-Hz 신호를 안정적으로 추적하기 위해 10ms의 PIT(Predetection Integration Time)와 비트동기를 고려한 Coherent 방식을 적용한 반송파 위상추적루프를 설계한다. 이렇게 설계된 신호추적루프의 성능을 검증하기 위해 항체의 동적환경과 위성신호 크기를 묘사해줄 수 있는 시뮬레이터를 이용하여 위성신호 추적성능을 시험하고 결과를 분석한다.

• Journal of IKEEE
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• v.13 no.1
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• pp.30-35
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• 2009

A new controller which can achieve the asymptotic tracking is proposed for the nonlinear system having a uncertainty in the input coefficient. A high gain observer is used to estimate the state variables when the nonlinear system has a modeling uncertainty. A variable structure control is used to achieve an asymptotic tracking, while ultimate boundness was achieved in the previous work. A Lyapunov analysis is used to justify the our proposal. The performance of proposed method is demonstrated via simulation.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.29 no.8
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• pp.640-647
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• 2018

This study analyzes the tracking accuracy(tracking errors) of fighter radar. Measurement error, detection failure, and radar cross section(RCS) fluctuation in radar measurements degrade the measurement quality and hence affect the tracking accuracy. Therefore, these radar measurement characteristics need to be considered when analyzing the tracking accuracy. In this paper, a method for analyzing the tracking accuracy is proposed; this method considers the detection error, detection probability, and RCS fluctuation. Results from experiments conducted with the proposed method show that the detection probability and RCS fluctuation affect tracking accuracy.

• Journal of the Institute of Electronics and Information Engineers
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• v.52 no.9
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• pp.125-131
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• 2015

The simulation programs with the kalman filter for the naval Electro Optical Tracking System(EOTS) is presented. We achieve that the dependency tracking aiming systems performance of EOTS can be enhanced by minimizing the target information error which including transfer delay and measurement. According to our experiment results, kalman filter can be used for various electro optical systems to eliminate error value.

• Bulletin of the Korean Space Science Society
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• 2003.10a
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• pp.68-68
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• 2003

본 논문은 별 추적기의 여러 가지의 성능변수 중에 광행차가 성능에 미치는 영향을 연구하였다. 일반적으로 광행차는 별 추적기의 저주파오차로 작용하며, 별 추적기 좌표계에서 최대 27" 정도의 성능을 감소시킨다. 지구가 태양 주위를 공전함으로써 야기되는 광행차는 약 21"이며, 줄리안 데이트를 통해서 보정이 가능하며, 관성 좌표계에서 지구 저궤도 위성이 궤도운동을 함으로 야기되는 광행차 오차는 약 6" 이며, 궤도정보를 통해서 보정이 가능하다. 이를 보정하기 위해서, 보정 알고리즘을 구현하여 다목적 실용위성 자세제어계 성능해석 소프트웨어를 통해서 검증을 하였다.

• Journal of Korea Water Resources Association
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• v.43 no.2
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• pp.153-165
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• 2010

Large-Scale Particle Image Velocimetry (LSPIV) is an extension of particle image velocimetry (PIV) for measurement of flows spanning large areas in laboratory or field conditions. LSPIV is composed of six elements - seeding, illumination, recording, image transformation, image processing, postprocessing - based on PIV. Possible error elements at each step of Mobile LSPIV (MLSPIV), which is a mobile version of LSPIV, in field applications are identified and summarized the effect of the errors which were quantified in the previous studies. The total number of elemental errors is 27, and five error sources were evaluated previously, seven elemental errors are not effective to the current MLSPIV system. Among 15 elemental errors, four errors - sampling time, image resolution, tracer, and wind - are investigated through an experiment at a laboratory to figure out how those errors affect to velocity calculation. The analysis to figure out the effect of the number of images used for image processing on the velocity calculation error shows that if over 50 images or more are used, the error due to it goes below 1 %. The effect of the image resolution on velocity calculation was investigated through various image resolution using digital camera. Low resolution image set made 3 % of velocity calculation error comparing with high resolution image set as a reference. For the effect of tracers and wind, the wind effect on tracer is decreasing remarkably with increasing the flume bulk velocity. To minimize the velocity evaluation error due to wind, tracers with high specific gravity is favorable.

• Journal of the Institute of Electronics Engineers of Korea SC
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• v.39 no.2
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• pp.166-175
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• 2002

In this paper. we predict tracking performance of the probabilistic strongest neighbor filter (PSNF). The PSNF is known to be consistent and superior to the probabilistic data association filter (PDAF) in both performance and computation. The PSNF takes into account the probability that the measurement with the strongest intensity in the neighborhood of the predicted target measurement location is not target-originated. The tracking performance of the PSNF is quantified in terms of its estimation error covariance matrix. The estimation error covariance matrix is approximately evaluated by using the hybrid conditional average approach (HYCA). We performed numerical experiments to show the validity of our performance prediction.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.17 no.11
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• pp.294-301
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• 2016

Recently, the solar tracker has been used to improve the efficiency of solar energy. Solar tracking technologies are classified into the sensor-based method, the program-based method, and the hybrid method. Solar trackers using an AC motor and CdS sensor are low in cost, but the precision of the positions is low, owing to the inertia of the motor and the scattering of sunlight. To compensate for the low precision, we implement a CdS sensor module and propose an AC motor control method using error value. To evaluate the performance of the solar tracker, we implemented a solar water heater. From the experimental results, the solar tracker can achieve ${\pm}2mm$ accuracy for sun, can satisfy ${\pm}15mm$ as a limited error value, and provides a 32% performance enhancement in KSB8202 criteria.

• Journal of Korea Water Resources Association
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• v.42 no.10
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• pp.891-896
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• 2009

The puff models have been developed to simulate the advection-diffusion processes of dredging suspended solids, either alone or in combination with Eulerian models. Computational efficiency and accuracy are of prime importance in designing these hybrid approaches to simulate a pollutant discharge, and we characterize two relatively simple Lagrangian techniques in this regard: forward Gaussian puff tracking (FGPT), and backward Gaussian puff tracking (BGPT). FGPT and BGPT offer dramatic savings in computational expense, but their applicability is limited by accuracy concerns in the presence of spatially variable flow or diffusivity fields or complex no-flux or open boundary conditions. For long simulations, particle and/or puff methods can transition to an Eulerian model if appropriate, since the relative computational expense of Lagrangian methods increases with time for continuous sources. Although we focus on simple Lagrangian models that are not suitable to all environmental applications, many of the implementation and computational efficiency concerns outlined herein would also be relevant to using higher order particle and puff methods to extend the near field.