• Bulletin of the Korean Space Science Society
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• 2004.04a
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• pp.86-86
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• 2004

다목적 실용위성 1호의 데이터를 이용하여 관측기간인 2000년 6월 28일에서 2001년 8월1일까지의 고도 685km, 22:50LT(Local Time) 이온층을 조사하였다. 데이터는 이온층 측정 센서(Ionospheric Measurement Sensor)로부터 얻은 전자 온도와 전자 밀도를 이용하였으며, 자기 위도로 -60$^{\circ}$-+60$^{\circ}$ 사이의 중ㆍ저위도의 값을 분석하였다. 관측 기간은 지자기 변화를 나타내는 Kp index나 태양 활동을 나타내는 F10.7이 크게 변화한 태양 극대기 기간으로, 이중 일변화의 F10.7을 통해 전자 온도와 전자 밀도의 변화를 조사하였다. (중략)

• Bulletin of the Korean Space Science Society
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• 1998.10a
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• pp.29.1-29
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• 1998

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2011.06a
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• pp.27-28
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• 2011

A solar flares have the 11-year cycle and release a large energy which may produce coronal mass ejections (CME). The NOAA (National Oceanic and Atmospheric Administration) predicted that the sun spot activity will be maximized in 2013-2014. A strong solar flare can cause the disturbance of global positioning system including various communication of TV, radio broadcasting. The actual solar storm in 1989 caused power outages in Canada during 9 hours and about 600 million people had experienced a blackout. Such a solar storm can shorten the GPS satellite's life span about 5 to 10 years which can be resulted in economic loss considering the amount of multi-billion won. This paper analyzed the recent solar storm of X-class occurred on 15th of February about 10:45 this year that was reached Korea (Bohyun observatory) on 18th of February about 10:30 (local time), and compared with the data of before and after a week. The proton data of 18th of February considered that the solar strom reached on earth showed a fluctuation compared to the data of before and after a week. The positioning results at Daejeon also showed higher positioning error compared to the data of before and after a week results.

• Journal of Navigation and Port Research
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• v.35 no.6
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• pp.477-482
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• 2011

Solar flares have the 11-year cycle and release a large energy which may produce coronal mass ejections (CME). The NOAA (National Oceanic and Atmospheric Administration) predicted that the sun spot activity will be maximized in 2013-2014. A strong solar flare can cause the disturbance of global positioning system including various communication of TV, radio broadcasting. The actual solar storm in 1989 caused power outages in Canada during 9 hours and about 600 million people had experienced a blackout. Such a solar storm can shorten the GPS satellite's life span about 5 to 10 years which can resulted in economic loss considering the amount of multi-billion won. This paper analyzed the influence of recent X-class solar storm occurred on 15th of February about 10:45 this year that was reached Korea (Bohyun observatory) on 18th of February about 10:30 (01:30 - UTC), and compared with the data before and after a week. The proton data of 18th of February considered that the solar storm reached on earth showed a fluctuation compared to the data before and after a week. The positioning results at Daejeon and Seoul of Korea also showed higher positioning error compared to the data before and after a week results.

• Satellite Communications and Space Industry
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• v.10 no.1 s.24
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• pp.144-155
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• 2002

• Bulletin of the Korean Space Science Society
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• 1998.10a
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• pp.61-61
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• 1998

• The Bulletin of The Korean Astronomical Society
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• v.20
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• pp.17.1-17.1
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• 1995

• The Science & Technology
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• s.528
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• pp.78-81
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• 2013

• Journal of Astronomy and Space Sciences
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• v.23 no.2
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• pp.135-142
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• 2006

The extension of sunspot number series and auroral observations backward in time is of considerable interest for dynamo theory, solar activity and climate research. It was known that the Maunder minimum corresponded to a unusual cold so called little ice age in Europe and the appearance of sunspot had a close relation to the occurrence of aurora. Therefore we have examined ancient records of sunspots and aurorae with indirect solar proxies during this period and have studied for the features and peculiarities of solar activity with the relation of the climate variation.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.10
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• pp.40-50
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• 2003

The operational orbit evolution of the KOMPSAT-l over 3 years was analyzed. During LEOP, four orbit maneuvers were performed to obtain the optimized orbit and eight safe-hold modes happened. The effects of unpredictable occurrence of the safe-hold mode and the highest solar activity on the orbit evolution during the mission life were analyzed. The comparison of orbital elements between long-term predicted orbit and determined orbit from observed data was also performed. The operational orbit started from the optimized one was evolved within the boundary of the designed mission orbit except altitude and it was verified the sun-synchronous orbit was successfully maintained.