• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.178.2-178.2
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• 2012

정지궤도위성은 발사체에서 위성이 분리된 이후 천이궤도로부터 원하는 목표궤도로 궤도전이를 해야 한다. 또한 임무기간동안 궤도상에서 다양한 교란을 겪게 되며 이로 인해 시간이 증가함에 따라 위성의 위치가 변화하게 된다. 정지궤도위성은 이러한 궤도전이 및 궤도상 위치변화를 제어하기 위한 추진시스템을 장착하고 임무기간에 걸쳐 요구되는 추진제를 탑재해야 한다. 위성의 설계 초기에는 추정되는 위성의 건조질량을 기반으로 하여 궤도전이와 궤도상 임무에 필요로 하는 추진제 버짓을 계산하고 이를 토대로 하여 위성 시스템 설계를 진행한다. 또한 발사체별로 발사체의 성능과 발사장에 따라 근지점고도와 발사 경사각이 모두 상이하므로 발사체가 정해지지 않은 상태에서 발사체별 추진제 버짓을 계산, 비교하고 추진 시스템의 탱크가 이를 모두 수용할 수 있는지 분석하는 것이 중요하다. 본 논문에서는 정지궤도복합위성의 추정 건조질량과 임무분석을 통해 주어진 ${\Delta}V$와 각 발사체별 궤도전이에 필요한 ${\Delta}V$를 바탕으로 하여 발사체별 추진제버짓을 계산하였고 이를 비교검토 하였다. 이후 이러한 기본 자료를 바탕으로 하여 정지궤도복합위성 추진시스템의 추진제 수용가능 여부, 건조질량 증가 여유 등 기본설계를 진행할 수 있다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.4
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• pp.384-392
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• 2008

Design sketch of electrical power system, mass, and cost of a new satellite is an inevitable step preceding the full-scale development of the satellite. In this paper, major features of recently developed conceptual design tools of satellites are investigated. And, based on the surveying results, we summarize the conceptual design procedure of satellites. The required electrical power to support the operation of the payload mission determines the size of solar panel and battery. The mass of the integrated system and subsystems is then estimated based on the database of the previously developed satellites. Cost can also be roughly estimated using the database without consideration of complex calculations.

• Journal of Aerospace System Engineering
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• v.16 no.5
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• pp.26-34
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• 2022

The propulsion system of geostationary orbiting satellites is typically used to raise the orbit into a transfer orbit, maintain the orbital position in the south/north, east/west direction in regular operation, and accumulate momentum in the south/north and east/west direction. Recently, when an electric propulsion system is used in a geostationary orbit satellite, the payload capacity can be increased by about 40% compared to a chemical propulsion system. However, despite these advantages, using an electric propulsion system has several limitations that should apply to all geostationary orbiting satellites. This paper discusses the operational constraints to consider when developing an indigenous geostationary satellite using a fully electric propulsion, radiation exposure, and control mechanism design due to unit displacement and floating ground-design. A high-voltage control unit for electric drives were analyzed.

• Korean Journal of Remote Sensing
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• v.33 no.5_3
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• pp.855-866
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• 2017

Several research cases using remote sensing methods to analyze changes of storage and dynamics of groundwater aquifer were reviewed in this paper. The status of groundwater storage, in an area with regional scale, could be qualitatively inferred from geological feature, surface water altimetry and topography, distribution of vegetation, and difference between precipitation and evapotranspiration. These qualitative indicators could be measured by geological lineament analysis, airborne magnetic survey, DEM analysis, LAI and NDVI calculation, and surface energy balance modeling. It is certain that GRACE and InSAR have received remarkable attentions as direct utilization from satellite data for quantification of groundwater storage and dynamics. GRACE, composed of twin satellites having acceleration sensors, could detect global or regional microgravity changes and transform them into mass changes of water on surface and inside of the Earth. Numerous studies in terms of groundwater storage using GRACE sensor data were performed with several merits such that (1) there is no requirement of sensor data, (2) auxiliary data for quantification of groundwater can be entirely obtained from another satellite sensors, and (3) algorithms for processing measured data have continuously progressed from designated data management center. The limitations of GRACE for groundwater storage measurement could be defined as follows: (1) In an area with small scale, mass change quantification of groundwater might be inaccurate due to detection limit of the acceleration sensor, and (2) the results would be overestimated in case of combination between sensor and field survey data. InSAR can quantify the dynamic characteristics of aquifer by measuring vertical micro displacement, using linear proportional relation between groundwater head and vertical surface movement. However, InSAR data might now constrain their application to arid or semi-arid area whose land cover appear to be simple, and are hard to apply to the area with the anticipation of loss of coherence with surface. Development of GRACE and InSAR sensor data preprocessing algorithms optimized to topography, geology, and natural conditions of Korea should be prioritized to regionally quantify the mass change and dynamics of the groundwater resources of Korea.