• 대한원격탐사학회지
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• 제35권6_1호
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• pp.895-905
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• 2019

현재 현업에서 사용되고 있는 상용 무인기 영상처리 소프트웨어는 카메라 캘리브레이션 정보나 영상 전체에 대한 블록 번들조정 정확도만 제공할 뿐 스테레오 페어의 실제 도화 가능여부에 대한 정확도는 거의 제공하지 않는다. 본 논문에서는 무인기 영상처리 소프트웨어에서 산출된 표정요소를 사용하여 도화품질을 산출하고 실제 도화기에 적용하여 도화품질의 신뢰성에 대해서 분석하였다. 도화품질은 Y시차 정확도, 상대모델 정확도, 절대모델 정확도의 3가지 정확도로 정의하였다. Y시차 정확도는 스테레오 페어간 입체시 여부를 판단할 수 있는 정확도이다. 상대모델 정확도는 모델 좌표계 상에서 스테레오 페어간 상대적인 번들조정 정확도이다. 절대모델 정확도는 절대 좌표계에서 번들조정 정확도이다. 실험데이터는 도심지를 대상으로 회전익에서 취득된 GSD 5 cm급의 영상 723장을 사용하여 도화품질을 분석하였다. 연구진이 개발한 기술을 사용해 예측한 상대모델 정확도와 실제 도화기에서 관측한 정확도의 최대오차는 0.11 m로 정밀한 결과를 보여 주었다. 절대모델 정확도도 마찬가지로, 도화기에서 관측한 정확도의 최대오차는 0.16 m로 정밀한 결과를 보여주었다.

• Imaging Science in Dentistry
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• 제34권1호
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• pp.13-18
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• 2004

Purpose : This study was to evaluate the influence of slice thickness of computed tomography (CT) and rapid protyping (RP) type on the accuracy of 3-dimensional medical model. Materials and Methods: Transaxial CT data of human dry skull were taken from multi-detector spiral CT. Slice thickness were 1, 2, 3 and 4 mm respectively. Three-dimensional image model reconstruction using 3-D visualization medical software (V-works /sup TM/ 3.0) and RP model fabrications were followed. 2-RP models were 3D printing (Z402, Z Corp., Burlington, USA) and Stereolithographic Apparatus model. Linear measurements of anatomical landmarks on dry skull, 3-D image model, and 2-RP models were done and compared according to slice thickness and RP model type. Results: There were relative error percentage in absolute value of 0.97, 1.98,3.83 between linear measurements of dry skull and image models of 1, 2, 3 mm slice thickness respectively. There was relative error percentage in absolute value of 0.79 between linear measurements of dry skull and SLA model. There was relative error difference in absolute value of 2.52 between linear measurements of dry skull and 3D printing model. Conclusion: These results indicated that 3-dimensional image model of thin slice thickness and stereolithographic RP model showed relative high accuracy.

• 농업과학연구
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• 제49권4호
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• pp.823-835
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• 2022

In this study, the feasibility of alternative tractor Roll Over Protective Structure (ROPS) designed to evaluate conditions required for testing was confirmed. In accordance with Organization for Economic Cooperation and Development (OECD) code 4, the required load energy of the tractor ROPS was determined. First, the tractor ROPS test was performed and a repeated test was performed using a simplified ROPS as an alternative tractor ROPS. The test procedure is first rearward, second lateral, and last forward based on ROPS. The load test device consists of a load cell that measures force and a LVDT that measures deformation. Precision was confirmed by calculating the relative standard deviation of the simplified ROPS repeated test. Accuracy was analyzed by calculating the mean relative error between the mean measured values in the simplified ROPS test and the tractor ROPS test. As a result, the relative standard deviation was less than 2.5% for force and 3.3% for maximum deformation overall, showed the highest precision in lateral load. The mean relative error value for force measured at the lateral load of simplified ROPS was 0.5%, showing the highest accuracy. In the front load test, the mean relative error of maximum deformation was 20.5%, showing the lowest accuracy. The mean relative error (MRE) was high in the forward load test was because of structural factors of the ROPS. The simplified ROPS model is expected to save money and time spent preparing tractors.

• Journal of Astronomy and Space Sciences
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• 제32권4호
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• pp.387-393
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• 2015

This study presents a precise relative navigation algorithm using both laser and Global Positioning System (GPS) measurements in real time. The measurement model of the navigation algorithm between two spacecraft is comprised of relative distances measured by laser instruments and single differences of GPS pseudo-range measurements in spherical coordinates. Based on the measurement model, the Extended Kalman Filter (EKF) is applied to smooth the pseudo-range measurements and to obtain the relative navigation solution. While the navigation algorithm using only laser measurements might become inaccurate because of the limited accuracy of spacecraft attitude estimation when the distance between spacecraft is rather large, the proposed approach is able to provide an accurate solution even in such cases by employing the smoothed GPS pseudo-range measurements. Numerical simulations demonstrate that the errors of the proposed algorithm are reduced by more than about 12% compared to those of an algorithm using only laser measurements, as the accuracy of angular measurements is greater than $0.001^{\circ}$ at relative distances greater than 30 km.

• Journal of Astronomy and Space Sciences
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• 제33권1호
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• pp.45-54
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• 2016

This study developed an approach for improving Carrier-phase Differential Global Positioning System (CDGPS) based realtime satellite relative navigation by applying laser baseline measurement data. The robustness against the space operational environment was considered, and a Synthetic Wavelength Interferometer (SWI) algorithm based on a femtosecond laser measurement model was developed. The phase differences between two laser wavelengths were combined to measure precise distance. Generated laser data were used to improve estimation accuracy for the float ambiguity of CDGPS data. Relative navigation simulations in real-time were performed using the extended Kalman filter algorithm. The GPS and laser-combined relative navigation accuracy was compared with GPS-only relative navigation solutions to determine the impact of laser data on relative navigation. In numerical simulations, the success rate of integer ambiguity resolution increased when laser data was added to GPS data. The relative navigational errors also improved five-fold and two-fold, relative to the GPS-only error, for 250 m and 5 km initial relative distances, respectively. The methodology developed in this study is suitable for application to future satellite formation-flying missions.

• 한국측량학회지
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• 제30권5호
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• pp.459-466
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• 2012

전리층에 의한 신호지연은 SA 해제이후 GPS 측위에 가장 큰 오차 요인이다. 전리층 오차는 이중주파수 수신기를 이용할 경우 무전리층 조합으로 쉽게 제거할 수 있지만 단일주파수 수신기는 무전리층 조합을 수행할 수 없기 때문에 전리층 오차를 쉽게 제거할 수 없다는 단점이 존재한다. 따라서 이 연구에서는 단일주파수 사용자를 위한 격자형 지역 전리층 모델을 개발하였다. 개발된 지역 전리층 모델을 평가하기 위해 IGS의 전지구 모델과 비교하였으며 그 결과 열흘 평균 3.8 TECU의 RMSE를 나타내었다. 그리고 측위 정확도에 미치는 영향을 평가하기 위해 생성된 지역 전리층 모델을 적용하여 L1 관측치만을 이용한 중 장기선 상대측위를 수행하였다. 전리층과 대류권 오차를 보정한 결과 두 오차를 보정하기 전의 측위 결과와 비교하여 평균 46.7%의 측위 정확도가 향상되었으며 대류권 오차만 보정한 측위 결과와 비교하여 전리층 오차 보정 후에는 평균 14.5%의 측위 정확도가 향상되었다.

• Journal of Astronomy and Space Sciences
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• 제26권3호
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• pp.317-328
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• 2009

위성의 상대운동 모델은 두 위성 사이의 상대적인 운동을 기술하며, 위성편대비행 연구의 기본이 된다. 이 연구에서는 선형 및 비선형 상대운동 모델들의 정확도를 산출하고 이를 비교 분석하였다. 우선 모델의 정확도를 나타내는 '모델링 오차 지수(Modeling Error Index)'를 정의하였다. 다양한 주위성 궤도의 이심률과 두 위성 사이의 거리에 대해 모델링 오차 지수를 계산하여, 여러 궤도환경에 따른 기존의 여러 가지 상대운동 모델들의 정확도를 산출하였다. 여러 가지 상대운동 방정식들의 모델링 오차 지수는 주위성의 이심률의 크기, J2 섭동 고려 여부, 위성들의 상대 거리의 크기에 따라 달라진다. 이 연구에서 사용한 상대운동 모델의 정확도는 편대비행 동역학모델의 오차를 나타내므로, 이 연구 결과를 이용해서 주어진 편대비행 임무에 알맞은 모델을 선택하는 것이 가능하다.

• 한국농림기상학회지
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• 제14권4호
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• pp.269-276
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• 2012

작물모형 평가에 사용되거나 사용할 수 있는 9가지 지표를 소개하였으며 이들의 특징은 다음과 같다. efficiency of model (EF)와 index of agreement (d)은 dimension이 없고 관측수(n)에 의존적이지 않았으며, dimension에 대해서만 자유로운 것은 relative root mean square error (RRMSE), bias factor (Bf)와 accuracy factor (Af)이다. Root mean sqruar, mean error, mean absolute error들은 관측수와 dimension에 영향을 받기 때문에 판단 시 주의가 필요하다. 따라서 이들의 특징을 파악하여 목적에 맞게 모형의 성능을 파악하여야 한다.

• International Journal of Control, Automation, and Systems
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• 제6권2호
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• pp.180-185
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• 2008

A new method for relative error continuous and discrete time model order reduction is proposed. The reduction technique is based on two recently developed methods, namely frequency domain balanced truncation within a frequency bound and inner-outer factorization techniques. The proposed method is of interest for practical model order reduction because in this context it shows to keep the accuracy of the approximation as high as possible without sacrificing the computational efficiency. Numerical results show the accuracy and efficiency enhancement of the method.

• 자동차안전학회지
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• 제10권2호
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• pp.29-35
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• 2018

This paper presents a quantitative evaluation method and result of moving vehicle perception using automotive radar. It is also important to analyze the accuracy of the perception algorithm quantitatively as well as to accurately percept nearby moving vehicles for safe and efficient autonomous driving. In this study, accuracy of the automotive radar-based perception algorithm which is developed based on interacting multiple model (IMM) has been verified via vehicle tests on real roads. In order to obtain experimental data for quantitative evaluation, Long Range Radar (LRR) has been mounted on the front of the ego vehicle and Short Range Radar (SRR) has been mounted on the rear side of both sides. RT-range has been installed on the ego vehicle and the target vehicle to simultaneously collect reference data on the states of the two vehicles. The experimental data is acquired in various relative positions and velocity, and the accuracy of the algorithm has been analyzed according to relative position and velocity. Quantitative analysis is conducted on relative position, relative heading angle, absolute velocity, and yaw rate of each vehicle.