• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.42 no.5
• /
• pp.368-375
• /
• 2014

The Ground Based Augmentation System (GBAS) is influenced by environmental factors, making analysis in the installation region important. This study has proposed the sigma inflation of the B-value considering the satellite elevation angle and analyzed the Vertical Protection Level (VPL) of the H1 hypothesis. After collecting data that meet the environmental conditions of the installation region, sigma expansion coefficients by the unit of satellite elevation angle ($5^{\circ}$) have been estimated. The obtained results were functionalized through curve-fitting, and sigma inflation customized for the environmental conditions of the test region was proposed. Then, the characteristics were classified and analyzed depending on humidity and solar activities. According to the sigma inflation with respect to elevation angle analysis, changes in the size of sigma inflation factors by the difference of humidity were minor. However, the VPL under the satellite elevation angle-based sigma inflation met integrity. Also, considering the sigma inflation factor with respect to elevation angle, compared to existing methods, high-integrity and improved availability is confirmed by removing unnecessary margins in high elevation angle satellite.

• Journal of the Korea Society for Simulation
• /
• v.28 no.3
• /
• pp.75-82
• /
• 2019

A Satellite Communication (SATCOM), which is applied to various systems to communicate with other systems at the limited wired communication situation, is required to head at a stable point of the space, because this system uses a geostationary satellite. It is important to know satellite tracking heading angles such as elevation angle and azimuth angle for the immovable antenna's latitude, longitude, and altitude. Moreover, calculation of heading angle is critical for SATCOM antenna on a moving platform. In this study, a antenna heading angle calculation method is applied to compute elevation and azimuth angle for a SATCOM antenna and the heading angle simulation is executed for the Korea peninsula and surrounding areas. To verify this simulation, satellite tracking test is conducted using a SATCOM antenna which uses monopulse signal tracking method. The simulation is confirmed by comparing this test result with the simulation. And we make a suggestion for calculation of polarization angle of this antenna.

• Journal of Advanced Navigation Technology
• /
• v.22 no.6
• /
• pp.610-615
• /
• 2018

Globally, global navigation satellite system (GNSS) is being developed and operated in advanced countries. China's Beidou is developing rapidly, starting with global positioning system (GPS), which is the most representative system. In this paper, we analyze the visibility of Beidou satellite in Korea at present time to utilize rapidly changing Beidou. In this analysis, it is compared with GPS which is stable service. The results of the visibility analysis are based on the results of the mask angle (the low elevation satellite exclusion angle) and the result of the skyplot (a visual representation of the position of the satellite at the user location). Visibility analysis shows that the high elevation angle of Beidou satellite is higher than that of GPS satellite in Korea. In addition, GPS and Beidou's availability and positioning accuracy analysis are performed to confirm the effect of increasing elevation angle satellites. According to the results, Beidou is more effective than GPS in using high elevation satellites in Korea.

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

• The Journal of Korean Institute of Communications and Information Sciences
• /
• v.25 no.9A
• /
• pp.1313-1321
• /
• 2000

In recent years LEO(Low Earth Orbit) satellite communication systems have gained a lot of interest as high speed multimedia services by satellite are about to be provided. It is mandatory to use very efficient ECC(Error Correcting Code) to support high speed multimedia services over LEO satellite channel. Turbo codes developed by Berrou et al. in 1993 have been actively researched since it can achieve a performance close to the Shannon limit. In this paper, a LEO satellite channel model is adopted and the fading characteristics of LEO satellite channel are analyzed for the change of elevation angle in various propagation environments. The performance of turbo code is analyzed and compared to that of conventional convolutional code using the satellite channel model. In the simulation results using the Globalstar orbit constellations, performance of turbo codes shows 1.0~2.0dB coding gain compared to that of convolutional codes over all elevation angle and propagation environment ranges we have investigated. The performance difference resulting from the change of elevation angle in various propagation environments and the performance of different ECC are analyzed in detail, so that the results can be applied to choose an appropriate ECC scheme for various system environment.

• Journal of the Korean Society of Fisheries and Ocean Technology
• /
• v.25 no.1
• /
• pp.1-5
• /
• 1989

A number of studies for the improvement of the accuracy of NNSS fix were carried out previously. But most studies were done when a ship was stationary at the fixed position. To investigate the accuracy of NNSS fix affected by the error of ship's speed and course when a ship was moving, the computer simulation was performed by each satellite, passing direction of satellite, and elevation angle. The obtained results are summarized as follows: 1. When elevation angle and passing direction of satellite were constant, there were little difference in the accuracy of NNSS fix from among those. 2. The accuracy of NNSS fox caused by the error of ship's speed was in proportion to the absolute value of it without regard to the magnitude of ship's speed, and it also became different according to the ship's course. 3. When the error of ship's speed was constant, the accuracy of the fixed position became different according to the passing direction of the satellite. 4. When the ship's course was south or north, the error of NNSS fix was greater than that of east or west, and the higher the elevation angle of the satellite, the greater the error of the NNSS fix.

• The Proceeding of the Korean Institute of Electromagnetic Engineering and Science
• /
• v.4 no.3
• /
• pp.37-44
• /
• 1993

The earth station antenna operating on a GEO communication satellite is influenced by sun interference in the period of the spring or the autumn eqinox. Such phenomena are also undertaken by ray-bending phenomena in atmosphere. Therefore the prediction time of sun interference does not theoretically match actual interference time. In this paper, the actual sun interference time has been analyzed in consideration of ray-bending phenomenon, the size of main reflector of earth station antenna and elevation angle between an earth station antenna and a satellite. Ray-bending phenomenon in atmosphere is proved to be disregarded if the Mugungwha satellite is luanched in 1995. The analysis results are compared with actual measurement values of sun interference time at local earth stations and the two data are in accord well.

• Journal of the Korean Society of Fisheries and Ocean Technology
• /
• v.23 no.1
• /
• pp.18-24
• /
• 1987

For the purpose of getting the accuracy of NNSS fix, the continuous observation was performed to search the factors affecting the accuracy of NNSS fix, and then to examine their effects. The observation was made at Lat. $35^{\circ}'||'&'||'<\TEX>05'04"N, Long. '||'&'||'129^{\circ}'||'&'||'<\TEX> 02'13"E from 28th January to 20th July in 1985. Accuracy of the position fixed in accordance with the observation time, each satellite, elevation angle doppler count, passed direction of each satellite and the antenna height were analyzed. The results obtaines are summerized as follows: 1. The deflaetion error is reduced to 0.21 miles when the geodetic system of the calculating the position converted from WGS-72 to Bessel. 2. When the elevation angle of the mountain is high, or the range of the elevation angle of satellite is 20-70 degrees, the position fixed comes nearest the true position. 3. The position fixed is more accurate on the condition that doppler count is more than 21, and at night than in daytime. 4. The accuracy of the position fixed is more seriously affected when the input data of the antenna height has considerable errors. But there occures almost little difference in the accuracy of position according to each satellite.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
• /
• 2014.10a
• /
• pp.277-279
• /
• 2014

TEQC는 인공위성으로부터 수신한 데이터를 편집, 품질검사, 포맷변환하기 위한 소프트웨어이다. TEQC 품질검사를 사용하면 여러 결과파일이 생성되는데 이를 활용하여 DGPS기준국 전파수신 환경을 분석하였다. 특히 방위각, 앙각에 따른 장애물의 여부를 가능하다.

• 한국정보통신설비학회:학술대회논문집
• /
• 2003.08a
• /
• pp.12-15
• /
• 2003

이동체 탑재형 안테나는 특성상 소형화 및 신호 추적 시간 단축이 중요한 요소이다. 이러한 특성은 위상변위기를 이용한 전자적인 빔 조향 방식으로 한층 더 보완할 수 있다. 현재 이동체에서 주로 사용되고 있는 DBS (Direct Broadcasting Satellite) 수신용 안테나는 패치 및 슬롯 형태의 안테나 소자를 배열하여 사용한다. 하지만 이러한 안테나 소자는 전방위각에 대해 인공위성 방향(앙각 45도)에서 이득 손실이 있기 때문에 위상변위기를 이용한 빔 조향 방식에서 사용하기에는 문제점을 가지고 있다. 따라서 모든 방위각에 대해 앙각 45도에서 최대 이득 특성을 갖는 안테나 소자를 이용해 이득 손실을 줄이는 것은 큰 의미가 있다. 본 논문에서는 monopole 주변에 PBG(Photonic Band Gap) 구조를 구현함으로써 표면파를 억제하여 앙각 45도 방향에서 최대 이득 특성을 보이는 안테나 소자를 제안한다.