• 제목/요약/키워드: north/east error

검색결과 47건 처리시간 0.02초

A Study on the Longitudinal and Lateral Errors of Air Vehicle Heading for Auto-landing

  • Park, Ji Hee;Park, Hong Sick;Shin, Chul Su;Jo, Young-Wo;Shin, Dong-Ho
    • Journal of Positioning, Navigation, and Timing
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    • 제2권2호
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    • pp.115-121
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    • 2013
  • For the auto-landing operation of an air vehicle, the possibility of auto-landing operation should be first evaluated by testing the navigation performance through a flight test. In general, navigation performance is tested by analyzing north/east/down (NED) errors relative to reference equipment whose precision is about 8~10 times higher than that of a navigation system. However, to evaluate the auto-landing operation of an air vehicle, whether the air vehicle approaches a glide path aligned with the runway, within a specific error, needs to be examined rather than examining the north/east errors of the navigation system. Therefore, the longitudinal/lateral errors of air vehicle heading need to be analyzed. In this study, a method for analyzing the longitudinal/lateral errors of a navigation system was proposed as the navigation performance test method for evaluating the safety during the auto-landing of an air vehicle. Also, flight tests were performed six times, and the safety of auto-landing was examined by analyzing the performance using the proposed method.

GOSAT 기반의 동북아시아 CO2 분포도에 적용된 크리깅 기법의 비교평가 (Comparative Evaluation among Different Kriging Techniques applied to GOSAT CO2 Map for North East Asia)

  • 최진호;엄정섭
    • 환경영향평가
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    • 제20권6호
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    • pp.879-890
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    • 2011
  • The GOSAT (Greenhouse gases Observing SATellite) data provide new opportunities the most regionally complete and up-to-date assessment of $CO_2$. However, in practice, GOSAT records often suffer from missing data values mainly due to unfavorable meteorological condition in specific time periods of data acquisition. The aim of this research was to identify optimal spatial interpolation techniques to ensure the continuity of $CO_2$ from samples taken in the North East Asia. The accuracy among ordinary kriging (OK), universal kriging (UK) and simple kriging (SK) was compared based on the combined consideration of $R^2$ values, Root Mean Square Error (RMSE), Mean Error (ME) for variogram models. Cross validation for 1312 random sampling points indicate that the (UK) kriging is the best geostatistical method for spatial predictions of $CO_2$ in the East Asia region. The results from this study can be useful for selecting optimal kriging algorithm to produce $CO_2$ map of various landscapes. Also, data users may benefit from a statistical approach that would allow them to better understand the uncertainty and limitations of the GOSAT sample data.

2 차원 탐색 레이다를 위한 국부 항법 좌표계에서의 운동보상을 포함한 추적필터 (A Tracking Filter with Motion Compensation in Local Navigation Frame for Ship-borne 2D Surveillance Radar)

  • 김병두;이자성
    • 제어로봇시스템학회논문지
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    • 제13권5호
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    • pp.507-512
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    • 2007
  • This paper presents a tracking filter with ship's motion compensation for a ship-borne radar tracking system. The ship's maneuver is described by displacement and rotational motions in the ship-centered east-north frame. The first order Taylor series approximation of the measurement error covariance of the converted measurement is derived in the ship-centered east-north frame. The ship's maneuver is compensated by incorporating the measurement error covariance of the converted measurement and displacement of the position state in the tracking filter. The simulation results via 500 Monte-Carlo runs show that the proposed method follows the target successfully and provides consistent tracking performance during ship's maneuvers while the conventional tracking filter without ship motion compensation fails to track during such periods.

무궁화위성 2호의 동서위치유지 박스 설정에 관한 연구 (A Study on the East-West Station Keeping Box of Koreasat 2)

  • 이상철;김방엽;박봉규
    • 한국항공우주학회지
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    • 제31권9호
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    • pp.75-81
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    • 2003
  • 정지궤도 위성의 위치는 여러 외부 교란력에 의해서 끊임없이 움직이기 때문에 우주에서 한 점으로 정의할 수 없다. 따라서 정지궤도 위성의 통신방송과 같은 일반적 임무를 수행하기 위해서는 우주의 한정된 공간인 위치유지박스 내에 운용되어야 한다. 본 연구에서는 남북위치유지 오차보다 상대적으로 큰 동서 위치유지 박스를 설정하기 위해서 여러 오차들을 유도하여 정립하였다. 이를 이용하여 무궁화위성에서 사용하고 있는 7일의 위치유지주기를 검증하고 14일로 위치유지 주기를 늘릴 경우의 문제점을 분석하였다.

Ionospheric Modeling at North-East Asia using IGS sites

  • Choi, Byung-Kyu;Park, Jong-Uk;Lee, Sang-Jeong
    • 한국항해항만학회:학술대회논문집
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    • 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.2
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    • pp.195-198
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    • 2006
  • One of the major sources of error in precise GPS positioning since the turn-off the Selective Availability(SA) is the ionospheric propagation delay. For the last decades, a lot of the ionospheric researches based on a GPS network have been implemented throughout the world. Especially researches of the ionospheric modeling for Wide Area Argumentation System(WAAS) have been undertaken and published. In mid-latitude regions, typical spatial and temporal variations in ionospheric models delay tend to minimal. The developed ionospheric model calls for a 1.25 degree grid at latitudes and a 2.5 degree grid at longitudes. The precise grid TEC estimated by the inversion technique is also compared with global ionosphere maps(GIMs) which have been provided by several analysis centers(ACs). The results of initial investigations into the suitability of the proposed ionospheric modeling scheme in north-east Asia are presented.

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Ionospheric Modeling at North-East Asia using IGS sites

  • Choi, Byung-Kyu;Park, Jong-Uk;Lee, Sang-Jeong
    • 한국항해항만학회:학술대회논문집
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    • 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.2
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    • pp.199-202
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    • 2006
  • One of the major sources of error in precise GPS positioning since the turn-off the Selective Availability(SA) is the ionospheric propagation delay. For the last decades, a lot of the ionospheric researches based on a GPS network have been implemented throughout the world. Especially researches of the ionospheric modeling for Wide Area Argumentation System(WAAS) have been undertaken and published. In mid-latitude regions, typical spatial and temporal variations in ionospheric models delay tend to minimal. The developed ionospheric model calls for a 1.25 degree grid at latitudes and a 2.5 degree grid at longitudes. The precise grid TEC estimated by the inversion technique is also compared with global ionosphere maps(GIMs) which have been provided by several analysis centers(ACs). The results of initial investigations into the suitability of the proposed ionospheric modeling scheme in north-east Asia are presented.

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여름철 북서태평양 태풍발생 예측을 위한 통계적 모형 개발 (Prediction of the number of Tropical Cyclones over Western North Pacific in TC season)

  • Sohn, Keon-Tae;Hong, Chang-Kon;Kwon, H.-Joe;Park, Jung-Kyu
    • 한국데이터정보과학회:학술대회논문집
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    • 한국데이터정보과학회 2002년도 춘계학술대회
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    • pp.9-15
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    • 2002
  • This paper presents the seasonal forecasting of the occurrence of tropical cyclone (TC) over Western North Pacific (WNP) using the generalized linear model (GLM) and dynamic linear model (DLM) based on 51-year-data (1951-2001) in TC season (June to November). The numbers of TC and TY are predictands and 16 indices (the E1 Nino/Southern Oscillation, the synoptic factors over East asia and WNP) are considered as potential predictors. With 30-year moving windowing, the estimation and prediction of TC and TY are performed using GLM. If GLM forecasts have some systematic error like a bias, DLM is applied to remove the systematic error in order to improve the accuracy of prediction.

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지구동주기위성의 위치보전해석과 궤도결정 (Station Keeping Analysis and Orbit Determination of Feosynchronous Satellite)

  • 박수홍;조겸래
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1993년도 한국자동제어학술회의논문집(국내학술편); Seoul National University, Seoul; 20-22 Oct. 1993
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    • pp.783-787
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    • 1993
  • The dynamics for a two-body problem including perturbations due to nonspherical gravitation of the earth, gravitation of the sun and moon, radiation of the sun is studied. Orbit determination was performed by SVD filter. The simulation result shows that the characteristics of the satellite orbit have east-west and south-north drift. Therefore, the periodic magnitude of the control time and value in the view of the periodicity of error can be provided, and this result can be basic data to a station keeping problem with an orbit determination result.

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Characteristics of Summer Tropospheric Ozone over East Asia in a Chemistry-climate Model Simulation

  • Park, Hyo-Jin;Moon, Byung-Kwon;Wie, Jieun
    • 한국지구과학회지
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    • 제38권5호
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    • pp.345-356
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    • 2017
  • It is important to understand the variability of tropospheric ozone since it is both a major pollutant affecting human health and a greenhouse gas influencing global climate. We analyze the characteristics of East Asia tropospheric ozone simulated in a chemistry-climate model. We use a global chemical transport model, driven by the prescribed meteorological fields from an air-sea coupled climate model simulation. Compared with observed data, the ozone simulation shows differences in distribution and concentration levels; in the vicinity of the Korean Peninsula, a large error occurred in summer. Our analysis reveals that this bias is mainly due to the difference in atmospheric circulation, as the anomalous southerly winds lead to the decrease in tropospheric ozone in this region. In addition, observational data have shown that the western North Pacific subtropical high (WNPSH) reduces tropospheric ozone across the southern China/Korean Peninsula/Japan region. In the model, the ozone changes associated with WNPSH are shifted westward relative to the observations. Our findings suggest that the variations in WNPSH should be considered in predicting tropospheric ozone concentrations.

통신위성에 작용하는 섭동력의 영향평가와 궤도결정 (A Study on Perturbation Effect and Orbit Determination of Communication Satellite)

  • 박수홍
    • 한국정밀공학회지
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    • 제9권3호
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    • pp.157-164
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    • 1992
  • This study concerns about the orbit prediction and orbit determination of Korean future communication satellite, called 'Moogunghwa", which will be motioned in the geo-stationary orbit. Perturbation effect on the satellite orbit due to nonspherical gravitation of the earth, gravitation of the sun and moon, radiation of sun, drag of the atmosphere was investigated. Cowell's method is used for orbit prediction. Orbit determination was performed by using Extended Kalman Filter which is suitable for real-time orbit determination. The result shows that the chacteristics of the satellite orbit has east-west and south-north drift. So the periodic control time and control value in the view of the periodic of error can be provided. The orbit determination demonstrated the effectiveness since the convergence performance on the positon and velocity error, and state error standard deviation is reasonable.able.

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