• Title/Summary/Keyword: Satellite Structure

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A Study on Optical Seemless of Discrete LED panels with Focusing Effect of prism Structure (프리즘 구조의 집광효과를 이용한 이산형 LED 패널의 광학적 연속성 구현에 관한 연구)

  • Cho, Sung-Hwan;Kim, Eung-Bo;Choi, Won-Seok;Joung, Yeun-Ho
    • Journal of Satellite, Information and Communications
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    • v.12 no.2
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    • pp.11-14
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    • 2017
  • In this paper, we introduce a method of light focusing effect using prism structure to solve optical discontinuity of conventional external signage LED panels. The prims structures were patterned on a transparent polycarbonate substrate with MEMS and femto-second laser process. We have confirmed that the patterned prism structures on the substrate made artificial LED lights on empty space between the panels by light guide effect of the structure. The artificial light's lateral positions were controlled by thickness of polycarbonate substrate. This cost effective prim patterned transparent film can be utilized on digital signage LED panels to achieve good optical communication.

High Fidelity Calculation of Thermal Load in a Satellite Orbit (고정확도의 인공위성 궤도 열하중 계산 기법)

  • Kim, Min-Ki
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.10
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    • pp.898-906
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    • 2017
  • This paper discusses the efficient high fidelity calculation of external thermal loads of a spacecraft on its orbit. Thermal loads to a spacecraft consist of three major components, direct solar radiation, earth reflection of solar rays, and earth irradiation. With the assumption that both earth reflection and earth emission are diffuse, thermal loads from earth surface divided into pieces of segments to satellite surfaces are individually calculated and summed over. By using analytical integration of both reflected and emitted heat load by earth, high rate of numerical convergence is achieved and the results are even exactly calculated in special cases. Moreover, KD tree ray tracing is employed in the calculation of thermal load to determine whether the radiated ray is obstructed or not by satellite structure.

A Design of Mode-Coupler with a Pair of Slots for Ka Band Multi-Mode Monopulse Tracking System (Ka 대역 다중모드 모노펄스 추적 시스템을 위한 한 쌍의 슬롯(Slot)을 갖는 모드커플러 설계)

  • Kwon, Kun-Sup;Heo, Jong-Wan;Hwang, Ki-Min
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.26 no.2
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    • pp.158-164
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    • 2015
  • The main mission of OTM(On-The-Move) satellite communication system is to provide satellite communication service while moving on a vehicle. So it should have a capability to maintain a reliable communication channel when it travels at high speeds or in a severe fluctuation region. This paper presents a small-sized multi-mode monopulse structure applicable to OTM satellite communication system which has only single mode-coupler with a pair of slot using a feature of circular polarized received signal. And tracking error signal is defined using fundamental and high-order modes.

Dynamics Modeling and Simulation of Korean Communication, Ocean, and Meteorology Satellite

  • No, Tae-Soo;Lee, Sang-Uk;Kim, Sung-Ju
    • International Journal of Aeronautical and Space Sciences
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    • v.8 no.2
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    • pp.89-97
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    • 2007
  • COMS(Communication, Oceanography, and Meteorology Satellite) is the first Korean multi-purpose satellite which is planned to be deployed at the altitude of geosynchronous orbit above the Korean peninsular. Noting that COMS is composed of the main BUS structure, two deployable solar panels, one yoke, five reactions wheels, COMS is treated as a collection of 9 bodies and its nonlinear equations of motion are obtained using the multi-body dynamics approach. Also, a computer program is developed to analyze the COMS motion during the various mission phase. Quite often, the equations of motion have to be derived repeatedly to reflect the fact that the spacecraft dynamics change as its configuration, and therefore its degree of freedom varies. However, the equations of motion and simulation software presented in this paper are general enough to represent the COMS dynamics of various configurations with a minimum change in input files. There is no need to derive the equations of motion repeatedly. To show the capability of the simulation program, the spacecraft motion during the solar array partial and full deployment has been simulated and the results are summarized in this paper.

Object-oriented Information Extraction and Application in High-resolution Remote Sensing Image

  • WEI Wenxia;Ma Ainai;Chen Xunwan
    • Proceedings of the KSRS Conference
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    • 2004.10a
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    • pp.125-127
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    • 2004
  • High-resolution satellite images offer abundance information of the earth surface for remote sensing applications. The information includes geometry, texture and attribute characteristic. The pixel-based image classification can't satisfy high-resolution satellite image's classification precision and produce large data redundancy. Object-oriented information extraction not only depends on spectrum character, but also use geometry and structure information. It can provide an accessible and truly revolutionary approach. Using Beijing Spot 5 high-resolution image and object-oriented classification with the eCognition software, we accomplish the cultures' precise classification. The test areas have five culture types including water, vegetation, road, building and bare lands. We use nearest neighbor classification and appraise the overall classification accuracy. The average of five species reaches 0.90. All of maximum is 1. The standard deviation is less than 0.11. The overall accuracy can reach $95.47\%.$ This method offers a new technology for high-resolution satellite images' available applications in remote sensing culture classification.

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Inplementation of flooding simulation in coastal area based on 3D satellite images and Web GIS

  • Jo, Myung-Hee;Park, Hyeon-Cheol;Kim, Hyoung-Sub;Choi, Yong-Ki
    • Proceedings of the KSRS Conference
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    • v.1
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    • pp.166-169
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    • 2006
  • Our country's coast is vulnerable area to natural disaster which the repetitive damages occur every year including a loss of lives, the damage of facilities and erosion mostly except for the east coast because of a typhoon, tidal waves, sea water overflowing by topographic structure of low-lying gentle slope and shallow sea. However, as for prevention of natural disaster occurring every year, the situation is that it's centered on the restorationcentered measures and the general disaster prevention research to minimize damages at the time of disaster occurrence is insufficient. This study intendedlop t to devehe techniques possible for real time sampling of damage prediction areas on Web in order to support decision making for damage prevention and establishment of disaster prevention policy. For this, the thematic map was produced related to disaster based on high-resolution satellite picture, and the environmental DB similar to real world was constructed through topographic construction of three-dimension integrating the parts of land and the sea. In addition, the system was developed possible for the expression of damageable regions by real time grasp of dangerous regions at the time of disaster occurrence through over flowing simulation of three-dimension, and it's intended to prepare a basis to minimize damages to disaster situations through it.

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RF Interference Analysis and Verification in the Synthetic Aperture Radar Satellite System (영상레이더 위성시스템 구조물의 RF 간섭특성 분석 및 검증)

  • Jang, Jae-Woong;Kim, Tae-Yoon;Lim, Seong-Bin
    • Aerospace Engineering and Technology
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    • v.8 no.1
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    • pp.187-196
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    • 2009
  • Synthetic Aperture Radar(SAR) satellite system for broad-area imaging has RF systems including SAR radiating a high power, data link system transmitting the acquired image data from the SAR, TC&R(Telemetry, Command, and Ranging) to communicate with a ground segment to control a satellite. Each system transmits RF signal having various frequencies and radiates a high power, RS(Radiated Susceptibility) specification should be verified at an electronic unit mounted in satellite. RF interference can be happened because of non-linearity of a RF system. Therefore, we manufactured a structure model installed antennas which have a similar pattern with a real antenna, the effect by RF interference is analyzed and verified.

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Application of XML to Develop GUI within Satellite Imageries Search System (위성 영상 검색시스템의 GUI 개발을 위한 XML 적용)

  • Bu, Ki-Dong;Lee, Young-Ju
    • Journal of the Korean Association of Geographic Information Studies
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    • v.5 no.4
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    • pp.65-74
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    • 2002
  • The purpose of this study is to develop an XML based GUI that can search for satellite image information which is converted to XML data format and stored in the database server on the web, and modify and reuse data. In order to implement these functions efficiently, we used a DOM interface of XML that increases the efficiency of accessing the document structure. We used HTML and Java script programming to facilitate this interface. The system was applied to the management system of satellite images in the Research Institute of SFC at Keio University. Our results confirmed the technical functionalities.

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A Study on Battery Applying Technique for Stability of Satellite Power System (인공위성 전원 안정화를 위한 배터리 적용 기법 연구)

  • Jeon, Hyeon-Jin;Lee, Sangrok;Jeon, Moon-Jin;Lim, Seong-Bin
    • Aerospace Engineering and Technology
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    • v.12 no.2
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    • pp.7-13
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    • 2013
  • Power system in satellite shall produce stable outputs for successful mission accomplishment. However, unstability in overall electrical system is caused in a case where a load having a power profile with high-powered and micro-cycled pulse shape is connected to a satellite power system. In order to resolve this anomaly, "power system stabilization method using a battery" featured with simplicity can be applied, but there is a constraint to operate a battery in its normal operational conditions. In this paper, an effective interface structure for "power system stabilization method using a battery" is suggested and a battery protection algorithm for preventing over-charging and over-discharging is discussed.

Very Small Satellite Program for Expending the Space Technology Base: CanSat Competition (우주기술 저변확대를 위한 초소형위성 프로그램: 캔위성 경연대회)

  • Won, Su-Hee;Jun, Hyoung-Yoll;Kim, Sung-Hoon;Lee, Sang-Ryool
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.7
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    • pp.636-645
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    • 2012
  • This paper presented the CanSat competition as one of very small satellite programs for expending the space technology base. The CanSat was compared and characterized with a real satellite and the foreign CanSat competition cases and domestic CanSat development trends were summarized. On the basis of the above information, the organizational structure and function were suggested for domestic CanSat competition and the required technologies, such as satellite, launcher and ground station were described. And also, the prior plan for competition, including mission, education and schedule were suggested.