• Title/Summary/Keyword: RMS error

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Configuration of a 16-Element Array Antenna Design to Improve Signal Detection Performances (신호탐지 정확도를 높이기 위해 최적 배열형상을 고려한 16소자 배열안테나 설계)

  • Jang, Doyoung;Yoo, Sungjun;Wang, Jinchun;Lee, Jun-Yong;Choo, Hosung
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.30 no.6
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    • pp.438-444
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    • 2019
  • In this paper, we proposed a 16-element array antenna design to improve signal detection performances. The array antenna characteristics, such as mutual coupling, pattern deviation, and half power beamwidth of the active element, were examined to obtain an optimal spacing between individual elements. The single element of the array antenna consists of an indirect feed using L-shaped feed and shorted radiating patch to achieve a broadband operation. Root mean square(RMS) errors based on the incident angle of the signal were calculated to verify the signal detection performance of the proposed antenna. The results demonstrate that the proposed array antenna with optimal spacing is suitable for detecting interference signals with low RMS error.

A Feasibility Test on the DGPS by Correction Projection Using MSAS Correction

  • Yoon, Dong Hwan;Park, Byungwoon;Yun, Ho;Kee, Changdon
    • Journal of Positioning, Navigation, and Timing
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    • v.3 no.1
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    • pp.25-30
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    • 2014
  • Differential Global Positioning System-Correction Projection (DGPS-CP) algorithm, which has been suggested as a method of correcting pre-calculated position error by projecting range-domain correction to positional domain, is a method to improve the accuracy performance of a low price GPS receiver to 1 to 3 m, which is equivalent to that of DGPS, just by using a software program without changing the hardware. However, when DGPS-CP algorithm is actually realized, the error is not completely eliminated in a case where a reference station does not provide correction of some satellites among the visible satellites used in user positioning. In this study, the problem of decreased performance due to the difference in visible satellites between a user and a reference station was solved by applying the Multifunctional Transport Satellites (MTSAT) based Augmentation System (MASA) correction to DGPS-CP, instead of local DGPS correction, by using the Satellite Based Augmentation System (SBAS) operated in Japan. The experimental results showed that the accuracy was improved by 25 cm in the horizontal root mean square (RMS) and by 20 cm in the vertical RMS in comparison to that of the conventional DGPS-CP.

Sea State Hindcast for the Korean Seas With a Spectral Wave Model and Validation with Buoy Observation During January 1997

  • Kumar, B. Prasad;Rao, A.D.;Kim, Tae-Hee;Nam, Jae-Cheol;Hong, Chang-Su;Pang, Ig-Chan
    • Journal of the Korean earth science society
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    • v.24 no.1
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    • pp.7-21
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    • 2003
  • The state-of-art third generation wave prediction model WAM was applied to the Korean seas for a winter monsoon period of January 1997. The wind field used in the present study is the global NSCAT-ERS/NCEP blended winds, which was further interpolated using a bi-cubic spline interpolator to fine grid limited area shallow water regime surrounding the Korean seas. To evaluate and investigate the accuracy of WAM, the hindcasted wave heights are compared with observed data from two shallow water buoys off Chil-Bal and Duk-Juk. A detailed study has been carried with the various meteorological parameters in observed buoy data and its inter-dependency on model computed wave fields was also investigated. The RMS error between the observation and model computed wave heights results to 0.489 for Chil-Bal and 0.417 for Duk-Juk. A similar comparison between the observation and interpolated winds off Duk-Juk show RMS error of 2.28 which suggest a good estimate for wave modelling studies.

Modeling of PECVD Oxide Film Properties Using Neural Networks (신경회로망을 이용한 PECVD 산화막의 특성 모형화)

  • Lee, Eun-Jin;Kim, Tae-Seon
    • Journal of the Korean Institute of Electrical and Electronic Material Engineers
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    • v.23 no.11
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    • pp.831-836
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    • 2010
  • In this paper, Plasma Enhanced Chemical Vapor Deposition (PECVD) $SiO_2$ film properties are modeled using statistical analysis and neural networks. For systemic analysis, Box-Behnken's 3 factor design of experiments (DOE) with response surface method are used. For characterization, deposited film thickness and film stress are considered as film properties and three process input factors including plasma RF power, flow rate of $N_2O$ gas, and flow rate of 5% $SiH_4$ gas contained at $N_2$ gas are considered for modeling. For film thickness characterization, regression based model showed only 0.71% of root mean squared (RMS) error. Also, for film stress model case, both regression model and neural prediction model showed acceptable RMS error. For sensitivity analysis, compare to conventional fixed mid point based analysis, proposed sensitivity analysis for entire range of interest support more process information to optimize process recipes to satisfy specific film characteristic requirements.

A Comparison of CME Arrival Time Estimations by the WSA/ENLIL Cone Model and an Empirical Model

  • Jang, Soo-Jeong;Moon, Yong-Jae;Lee, Kyoung-Sun;Na, Hyeon-Ock
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.1
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    • pp.92.1-92.1
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    • 2012
  • In this work we have examined the performance of the WSA/ENLIL cone model provided by Community Coordinated Modeling Center (CCMC). The WSA/ENLIL model simulates the propagation of coronal mass ejections (CMEs) from the Sun into the heliosphere. We estimate the shock arrival times at the Earth using 29 halo CMEs from 2001 to 2002. These halo CMEs have cone model parameters from Michalek et al. (2007) as well as their associated interplanetary (IP) shocks. We make a comparison between CME arrival times by the WSA/ENLIL cone model and IP shock observations. For the WSA/ENLIL cone model, the root mean square(RMS) error is about 13 hours and the mean absolute error(MAE) is approximately 10.4 hours. We compared these estimates with those of the empirical model by Kim et al.(2007). For the empirical model, the RMS and MAE errors are about 10.2 hours and 8.7 hours, respectively. We are investigating several possibilities on relatively large errors of the WSA/ENLIL cone model, which may be caused by cone model velocities, CME density enhancement factor, or CME-CME interaction.

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Comparison of 3-D structures of Halo CMEs using cone models

  • Na, Hyeon-Ock;Moon, Y.J.;Jang, Soo-Jeong;Lee, Kyoung-Sun
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.1
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    • pp.95.1-95.1
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    • 2012
  • Halo coronal mass ejections (HCMEs) are major cause of geomagnetic storms and their three dimensional structures are important for space weather. In this study, we compare three cone models: an elliptical cone model, an ice-cream cone model, and an asymmetric cone model. These models allow us to determine the three dimensional parameters of HCMEs such as radial speed, angular width, and the angle (${\gamma}$) between sky plane and cone axis. We compare these parameters obtained from three models using 62 well-observed HCMEs from 2001 to 2002. Then we obtain the root mean square error (RMS error) between maximum measured projection speeds and their calculated projection speeds from the cone models. As a result, we find that the radial speeds obtained from the models are well correlated with one another (R > 0.84). The correlation coefficients between angular widths are less than 0.53 and those between ${\gamma}$ values are less than 0.47, which are much smaller than expected. The reason may be due to different assumptions and methods. The RMS errors of the elliptical cone model, the ice-cream cone model, and the asymmetric cone model are 213 km/s, 254 km/s, and 267 km/s, respectively. Finally, we discuss their strengths and weaknesses in terms of space weather application.

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Accuracy and Error Characteristics of SMOS Sea Surface Salinity in the Seas around Korea

  • Park, Kyung-Ae;Park, Jae-Jin
    • Journal of the Korean earth science society
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    • v.41 no.4
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    • pp.356-366
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    • 2020
  • The accuracy of satellite-observed sea surface salinity (SSS) was evaluated in comparison with in-situ salinity measurements from ARGO floats and buoys in the seas around the Korean Peninsula, the northwest Pacific, and the global ocean. Differences in satellite SSS and in-situ measurements (SSS errors) indicated characteristic dependences on geolocation, sea surface temperature (SST), and other oceanic and atmospheric conditions. Overall, the root-mean-square (rms) errors of non-averaged SMOS SSSs ranged from approximately 0.8-1.08 psu for each in-situ salinity dataset consisting of ARGO measurements and non-ARGO data from CTD and buoy measurements in both local seas and the ocean. All SMOS SSSs exhibited characteristic negative bias errors at a range of -0.50- -0.10 psu in the global ocean and the northwest Pacific, respectively. Both rms and bias errors increased to 1.07 psu and -0.17 psu, respectively, in the East Sea. An analysis of the SSS errors indicated dependence on the latitude, SST, and wind speed. The differences of SMOS-derived SSSs from in-situ salinity data tended to be amplified at high latitudes (40-60°N) and high sea water salinity. Wind speeds contributed to the underestimation of SMOS salinity with negative bias compared with in-situ salinity measurements. Continuous and extensive validation of satellite-observed salinity in the local seas around Korea should be further investigated for proper use.

Performance Analysis of Tactical Ballistic Missile Tracking Filters in Phased Array Multi-Function Radar (위상 배열 다기능 레이더의 탄도탄 추적 필터 성능 분석)

  • Jung, Kwang-Yong
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.23 no.8
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    • pp.995-1001
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    • 2012
  • This paper compares the performance of several tracking filters, namely, alpha-beta filter, Kalman filter and TBM tracking filter for ballistic target tracking problem using multi-function radar. Every of three tracking filters suggested was tested on simulator developed in accordance with TBM trajectory and MFR RSP measurement. The result shows the method using TBM tracking filter gives 75.3 % decreased velocity RMS error than alpha-beta filter. After initialization, the RMS error of range and velocity of the proposed filter is also smaller than the Kalman filter. Finally the proposed filter is suitable for high-speed TBM tracking due to the stable angle tracking accuracy.

A Study on the Development of Simple DGPS for the Coastal Survey (연안 해양 관측을 위한 간역 DGPS 개발 연구)

  • 이상룡;문동준;전호경
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • v.8 no.1
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    • pp.10-17
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    • 1996
  • A real time simple DGPS (SDGPS) for coastal survey is developed and in situ tested. While the accuracy of the system is almost the same as that of existing commercially available DGPS, it is very economical compared to the commercial ones. The RMS error of the positions fired by the system is estimated to be less than 2 m within the range of 30 km from the reference station. Even if the coordinates of the reference station are uncertain, they can be fixed, from the continuous GPS observation of one day, with the maximum error less than 1 m. The system is believed to be helpfully utilized to most of coastal surveys despite of some minor defects.

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Investigation of Long-Term Shoreline Changes Using Aerial Images (항공사진을 이용한 장기해안선변화 조사)

  • 정승진;김규한;편종근
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • v.16 no.1
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    • pp.10-17
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    • 2004
  • In this paper, the affine transformation method that is more simpler compare with digital orthophoto method is used analyzed the long-term shoreline change, and accuracy estimation was carried out. As a result of this study, it was able to check that the shoreline change on Namhangjin coast had eroded significantly compare with the past. Moreover, as a result of accuracy estimation, it shows that the RMS error around shoreline was about 1-2 m. In consideration that maximum allowable error shown in aerial photogrammetry specification is within 2 m, therefore, analysis results of shoreline change using affine transformation method on aerial images is reliable.