• 제목/요약/키워드: Satellite structure

검색결과 783건 처리시간 0.024초

삼각벡터구조를 이용한 고해상도 위성 단영상에서의 건물 높이 추출 (Building Height Extraction using Triangular Vector Structure from a Single High Resolution Satellite Image)

  • 김혜진;한동엽;김용일
    • 대한원격탐사학회지
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    • 제22권6호
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    • pp.621-626
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    • 2006
  • IKONOS나 QuickBird와 같은 고해상도 위성영상이 상용화됨에 따라 위성영상으로부터 3차원 건물 정보를 취득하기 위한 많은 연구가 진행되고 있다. 3차원 건물 높이를 추출하는 연구는 크게 스테레오 영상 기반의 연구들과 단영상 기반의 연구들로 나눌 수 있는데 센서 모델링을 수반하는 스테레오 영상 기반의 연구들은 그 과정이 복잡하고, 실제 스테레오 영상을 취득하기 위해서는 별도의 주문과 비용이 소요되는 등의 어려움이 따른다. 기존의 단영상을 이용한 건물 높이 추출 연구들은 대부분 DEM 등의 부가적인 데이터를 필요로 하며, 건물의 그림자 길이나 건물 지붕점과 바닥점 관측을 통해 높이를 추출하였다. 이러한 기법들은 도시지역과 같이 건물이 밀집한 지역에서는 적용하기 부적합하다. 이에 이태윤(2006)의 연구에서는 가상의 그림자 투영 기법을 이용하여 건물의 그림자가 다른 인공체에 드리운 경우에도 건물 높이 추출이 가능한 기법이 제안된 바 있으나 이 기법은 건물의 그림자 끝이 식별되지 않는 건물에는 적용이 불가능하다. 이에 본 연구에서는 고해상도 위성 단영상에서 보다 많은 건물 높이의 관측이 가능하도록 하는 삼각 벡터구조 기반의 새로운 기법을 제안하였다. 제안된 기법은 센서모델링 과정이나 부가적인 데이터 없이 간단히 구현 가능하며 디지타이징 과정에서 발생하는 오차를 줄일 수 있다.

군위성 송수신기용 기존 금속 도파관을 대체하는 DNG형 기판적층 도파관 공진기의 설계 (Design of DNG-type Substrate-Integrated-Waveguide Resonators to Replace the Conventional Metallic Waveguide for the Military Satellite Transceiver)

  • 강경석;양인규;강승택;이호섭;김형종
    • 전기학회논문지
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    • 제62권11호
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    • pp.1584-1589
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    • 2013
  • A new and significantly small guided and resonant structure is suggested to take over bulky metallic hollow waveguides used in military satellite transceivers. Below Ku-band, the conventional waveguides resulting in quite heavy transceivers will be replaced by the low profile SIW(substrate integrated waveguide) structures that are distinguished from the others in that the suggested ones have much lower cut-off frequencies by the circuital configuration of DNG(dobule negative) constitutive parameters and become even smaller than the other SIWs. The design scheme is validated by the circuit and full-wave simulations from the guided, resonant, and coupled structures. Besides, a bandpass filter as the suggested coupled structure is fabricated with a cheap substrate in a low-budget fabrication process and its frequency response is measured as verification of the purpose of the design.

수정 시뮬레이티드 어닐링에 의한 항공우주 구조물의 최적설계 (Optimization of Aerospace Structures using Reseated Simulated Annealing)

  • 류미란;지상현;임종빈;박정선
    • 한국전산구조공학회논문집
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    • 제18권1호
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    • pp.71-78
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    • 2005
  • 수정 시뮬레이티드어닐링은 Simulated Annealing(SA)가 확률 탐색 방법을 사용하기 때문에 수렴시간이 오래 걸리는 단점를 개선한 방법이다. 따라서 본 논문에서는 RSA와 SA을 트러스구조물과 인공위성구조물의 최적화에 적용하여 서로 비교하여 보았다. 최적화 예제로 10부재 트러스, 실제 응용예제로 인공위성구조물은 위성 상단 플랫폼과 추진모듈의 최적화를 수행하였다. 인공위성구조물의 최적화에서 응력과 고유진동수, 전단응력 등을 제한조건으로 고려하여 최적화를 수행하였다. 인공위성구조물의 최적화를 수행한 결과 RSA을 이용하여 다양한 인공위성 구조물의 최적화에 적용될 수 있음을 확인하였으며, 인공위성 구조물의 최적화에서 RSA가 SA보다 수렴속도가 향상되었음을 확인하였다.

인공위성발사체 상단부 진동환경시험을 위한 치구설계 (Vibration Fixture design for small satellite launch vehicle environment test)

  • 정호경;서상현;박순홍;장영순;이영무
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2007년도 춘계학술대회논문집
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    • pp.258-262
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    • 2007
  • Satellite launch vehicle is exposed to some dynamic environment during its flight. Particularly, the safety of launch vehicle structure is surely verified under vibration environment in low frequency range. Sine sweep test is generally performed to describe this low frequency vibration environment. Dynamic property of vibration fixture is considered to get the correct property of target object. This vibration fixture should really be an extension of the armature in the form of a very rigid structure that can transfer the required force at the required frequency. An optimum fixture would have its lower natural frequency about 50% higher than the highest required forcing frequency in order to avoid fixture resonances during the test. In this study, the vibration mode analysis considering the mass of target object to design the vibration fixture. And the modal test of vibration fixture is performed to conform the design.

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지지부 위치와 벽면 두께변화에 따른 구형 인공위성 추진제 탱크의 강도해석 (Stress Analysis of the Spherical Satellite Propellant Tank With Respect to the Change of Location of the Lug and Tank Wall Thickness)

  • 한근조;장우석;안성찬;심재준;전형용
    • 한국정밀공학회지
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    • 제15권3호
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    • pp.31-37
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    • 1998
  • The structure of satellite consists of six parts which are control system, power system, thermal control system, remote measurement command system, propellant system and thrust system. In these parts, propellant system consists of propellant tank and thrust device. What we want to perform is optimum design to minimize the weight of propellant tank. In order to design optimal propellant tank, several parameters should be adopted from the tank geometry like the relative location of the lug and variation of the wall thickness. The analysis was executed by finite element analysis for finding optimal design parameters. The structure was divided into three parts consisting of the initial thickness zone, the transitional Bone, and the weak zone, whose effects on the pressure vessel strength was investigated. Finally the optimal lug location and the three zone thickness were obtained and the weight was compared with the uniform thickness vessel.

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과학기술위성 3호 홀추력기 추진계 개발 (STSAT-3 Hall Thruster Propulsion System Development)

  • 조희근;유광선;차원호;이종섭;서미희;최원호;명로훈
    • 한국항공우주학회지
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    • 제38권8호
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    • pp.834-841
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    • 2010
  • 최신기술이 적용된 전구조 복합재 위성인 과학기술위성 3호 (STSAT-3)가 국내 최초로 개발 되었으며 2011년 발사예정이다. 모든 위성과 마찬가지로 과기 3호에는 다수의 탑재체가 탑재될 예정이며 그 주된 목적은 선진 우주기술의 과학적 검증에 있다. 제논 가스를 연료로 하는 홀추력기가 국내 최초로 개발되어 지상시험을 거친 후 과기3호에 탑재되었다. 본 연구는 홀추력기 개발에 적용된 전반적인 개발기술, 절차, 기능 및 환경시험에 대한 내용이며 선진 우주기술 획득 및 차후 위성개발을 위한 기술자료 축적에 그 중요성이 있다.

Si 선택적 성장을 위한 대형 CVD 반응기 내의 열 및 유동해석 (Analysis on the Flow and Heat Transfer in a Large Scale CVD Reactor for Si Epitaxial Growth)

  • 장연호;고동국;임익태
    • 반도체디스플레이기술학회지
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    • 제15권1호
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    • pp.41-46
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    • 2016
  • In this study, gas flow and temperature distribution in the multi-wafer planetary CVD reactor for the Si epitaxial growth were analyzed. Although the structure of the reactor was simplified as the first step of the study, the three-dimensional analysis was performed taking all these considerations of the revolution of the susceptor and the rotation of satellites into account. From the analyses, a reasonable velocity field and temperature field were obtained. However, it was found that analyses including the upper structure of the reactor were required in order to obtain more realistic temperature results. DCS mole fraction above the satellite surface and the susceptor surface without satellite was compared in order to check the gas species mixing. We found that satellite rotation helped gases to mix in the reactor.

도시 열환경 분석을 위한 공간정보 빅데이터 구축 (Construction of Spatial Information Big Data for Urban Thermal Environment Analysis)

  • 이준호;윤성환
    • 대한건축학회논문집:계획계
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    • 제36권5호
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    • pp.53-58
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    • 2020
  • The purpose of this study is to build a database of Spatial information Bigdata of cities using satellite images and spatial information, and to examine the correlations with the surface temperature. Using architectural structure and usage in building information, DEM and Slope topographical information for constructed with 300 × 300 mesh grids for Busan. The satellite image is used to prepare the Normalized Difference Built-up Index (NDBI), Normalized Difference Vegetation Index (NDVI), Bare Soil Index (BI), and Land Surface Temperature (LST). In addition, the building area in the grid was calculated and the building ratio was constructed to build the urban environment DB. In architectural structure, positive correlation was found in masonry and concrete structures. On the terrain, negative correlations were observed between DEM and slope. NDBI and BI were positively correlated, and NDVI was negatively correlated. The higher the Building ratio, the higher the surface temperature. It was found that the urban environment DB could be used as a basic data for urban environment analysis, and it was possible to quantitatively grasp the impact on the architecture and urban environment by adding local meteorological factors. This result is expected to be used as basic data for future urban environment planning and disaster prevention data construction.

Mechanical Design for an Optical-telescope Assembly of a Satellite-laser-ranging System

  • Do-Won Kim;Sang-Yeong Park;Hyug-Gyo Rhee;Pilseong Kang
    • Current Optics and Photonics
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    • 제7권4호
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    • pp.419-427
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    • 2023
  • The structural design of an optical-telescope assembly (OTA) for satellite laser ranging (SLR) is conducted in two steps. First, the results of a parametric study of the major design variables (e.g. dimension and shape) of the OTA part are explained, and the detailed structural design of the OTA is derived, considering the design requirements. Among the structural-shape concepts of various OTAs, the Serrurier truss concept is selected in this study, and the collimation of the telescope according to the design variables is extensively discussed. After generating finite-element models for different structural shapes, self-gravity analyses are performed. To minimize the deflection and tilt of the mirror and frame for the OTA under the limited design requirements, a parametric study is conducted according to design variables such as the shapes of the upper and lower struts and the spider vane. The structural features found in the parametric study are described. Finally, the OTA structure is designed in detail to maintain the optical alignment by balancing the gravity deflections of the upper and lower trusses using the optimal combination of the parameters. Additionally, thermal analysis of the optical telescope design is evaluated.

Multi-GNSS Standard Point Positioning using GPS, GLONASS, BeiDou and QZSS Measurements Recorded at MKPO Reference Station in South Korea

  • Choi, Byung-Kyu;Cho, Chang-Hyun;Cho, Jung Ho;Lee, Sang Jeong
    • Journal of Positioning, Navigation, and Timing
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    • 제4권4호
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    • pp.205-211
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    • 2015
  • The Global Navigation Satellite System (GNSS) is undergoing dramatic changes. Nowadays, much more satellites are transmitting navigation data at more frequencies. A multi-GNSS analysis is performed to improve the positioning accuracy by processing combined observations from different GNSS. The multi-GNSS technique can improve significantly the positioning accuracy. In this paper, we present a combined Global Positioning System (GPS), the GLObal NAvigation Satellite System (GLONASS), the China Satellite Navigation System (BeiDou), and the Quasi-Zenith Satellite System (QZSS) standard point positioning (SPP) method to exploit all currently available GNSS observations at Mokpo (MKPO) station in South Korea. We also investigate the multi-GNSS data recorded at MKPO reference station. The positioning accuracy is compared with several combinations of the satellite systems. Because of the different frequencies and signal structure of the different GNSS, intersystem biases (ISB) parameters for code observations have to be estimated together with receiver clocks in multi-GNSS SPP. We also present GPS/GLONASS and GPS/BeiDou ISB values estimated by the daily average.