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公开(公告)号：KR1020110074021A
公开(公告)日：2011-06-30
申请号：KR1020090130853
申请日：2009-12-24
Applicant: 한국항공우주연구원
CPC classification number: B64G5/00
Abstract: PURPOSE: A device for holding and handling the body panel of a satellite is provided to improve the efficiency and stability of an assembling process since the body panel of the satellite can be easily and stably mounted on a mounting surface. CONSTITUTION: A device for holding and handling the body panel of a satellite comprises a strong back, a lifting tool(20) and a trolley(30). The strong back is coupled to the body panel of the satellite. The lifting tool lifts and moves the strong back using a plurality of lifting strings(22). The trolley enables the strong back moved through the lifting tool to be mounted. The trolley rotates the mounted strong back.
Abstract translation: 目的：提供一种用于保持和处理卫星的身体面板的装置，以提高组装过程的效率和稳定性，因为卫星的身体面板可以容易且稳定地安装在安装表面上。 构成：用于保持和处理卫星的身体面板的装置包括强背，提升工具（20）和手推车（30）。 强大的后背连接到卫星的车身面板。 提升工具使用多个提升绳（22）升起并移动强力后背。 手推车使强力后背能够移动通过提升工具进行安装。 手推车旋转安装的强力背部。
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公开(公告)号：KR1020110064061A
公开(公告)日：2011-06-15
申请号：KR1020090120486
申请日：2009-12-07
Applicant: 한국항공우주연구원
Abstract: PURPOSE: A deflection compensation system for a satellite is provided to prevent the deflection of a satellite by supporting the satellite on a bogie for rotating the satellite. CONSTITUTION: A deflection compensation system for a satellite comprises a main body(310) which has a through hole(311) and is installed on a bogie for rotating a satellite, a screw(312) which is inserted and slid in the through hole, a worm wheel which is formed inside the main body and engaged with the screw, a worm which is formed inside the main body and engaged with the worm wheel, a handle(315) which is connected to the worm to rotate the worm, and a bracket(320) which is installed on the top of the screw and coupled with a satellite.
Abstract translation: 目的：提供一种用于卫星的偏转补偿系统，以通过将卫星支撑在用于旋转卫星的转向架上来防止卫星的偏转。 构成：用于卫星的偏转补偿系统包括具有通孔（311）并安装在用于旋转卫星的转向架上的主体（310），在通孔中插入和滑动的螺钉（312） 蜗轮，其形成在主体内部并与螺钉接合，蜗杆形成在主体内并与蜗轮啮合;手柄（315），其与蜗杆连接以旋转蜗杆;和 支架（320），其安装在螺钉的顶部并与卫星耦合。
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公开(公告)号：KR1020110058447A
公开(公告)日：2011-06-01
申请号：KR1020090115248
申请日：2009-11-26
Applicant: 한국항공우주연구원
IPC: G01M99/00
Abstract: PURPOSE: A weightlessness offering apparatus for a deployment test of a solar panel is provided to implement a perfect weightless state by allowing a support cable supporting the weight of a solar panel to slide along two axes. CONSTITUTION: A weightlessness offering apparatus for a deployment test of a solar panel comprises a pair of rails(100) which are arranged in parallel, first slide members(200) which are installed in the rails and slid along the rails, a guide rail(300) which connects the first slide members, a second slide member(400), and a support cable(500) which is connected to the second slide member and a solar panel and supports the weight of the solar panel.
Abstract translation: 目的：提供一种用于太阳能电池板部署测试的失重提供装置，通过支撑支撑太阳能电池板重量的支撑电缆沿两个轴线滑动来实现完美的失重状态。 构成：用于太阳能电池板部署试验的失重提供装置包括平行布置的一对轨道（100），安装在轨道中并沿轨道滑动的第一滑动构件（200），导轨 300，其连接第一滑动构件，第二滑动构件（400）和连接到第二滑动构件的支撑缆索（500）和太阳能面板，并且支撑太阳能面板的重量。
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公开(公告)号：KR100775989B1
公开(公告)日：2007-11-15
申请号：KR1020060133997
申请日：2006-12-26
Applicant: 한국항공우주연구원
CPC classification number: B64G1/66 , B64G1/222 , B64G2001/1035
Abstract: An apparatus for supporting a synthetic aperture radar of a satellite is provided to obtain a space for mounting other equipment and satisfy dynamic characteristics and quasi-static conditions. An apparatus for supporting a synthetic aperture radar of a satellite includes support frames(110), upper and lower platforms(120,130), side panels(140), a support bracket(150), and a hinge bracket(160). The support frames are disposed at corners of a hexagonal post. The upper and lower platforms are connected to upper and lower ends of the support frame to form upper and lower surfaces of the support apparatus. The side panels constitutes side surfaces of the hexagonal support apparatus. The support bracket is coupled to a center part of the support frame to fasten the synthetic aperture radar. The hinge bracket is coupled to the support frame to fasten the synthetic aperture radar.
Abstract translation: 提供一种用于支持卫星的合成孔径雷达的装置，以获得用于安装其他设备并满足动态特性和准静态条件的空间。 用于支撑卫星的合成孔径雷达的装置包括支撑框架（110），上和下平台（120,130），侧板（140），支撑支架（150）和铰链支架（160）。 支撑框架设置在六边形柱的角部。 上平台和下平台连接到支撑框架的上端和下端以形成支撑装置的上表面和下表面。 侧板构成六边形支撑装置的侧表面。 支撑托架联接到支撑框架的中心部分，以固定合成孔径雷达。 铰链支架联接到支撑框架，以固定合成孔径雷达。
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公开(公告)号：KR100775988B1
公开(公告)日：2007-11-15
申请号：KR1020060105606
申请日：2006-10-30
Applicant: 한국항공우주연구원
CPC classification number: B64G1/66 , B64G2001/1028
Abstract: An optical loading device of an observation satellite is provided to effectively absorb thermal load generated in various directions. An optical loading device of an observation satellite includes a coupling unit(500). The coupling unit includes a first coupling part(510), a second coupling part(530), and a blade(550). The first coupling part is coupled to a platform. The second coupling part is coupled to a main body of the observation satellite. The blade connects the first coupling part and the second coupling part. Fastening grooves(510a) are formed in horizontal directions of the first coupling part. Fastening grooves(530a) are formed in vertical directions of the second coupling part. The coupling unit is connected to a main body of the platform.
Abstract translation: 提供了一种观测卫星的光学加载装置，以有效吸收在各个方向产生的热负荷。 观测卫星的光学加载装置包括耦合单元（500）。 联接单元包括第一联接部分（510），第二联接部分（530）和叶片（550）。 第一耦合部分耦合到平台。 第二耦合部分耦合到观测卫星的主体。 叶片连接第一联接部分和第二联接部分。 紧固槽（510a）在第一联接部的水平方向上形成。 紧固槽（530a）在第二联接部的垂直方向上形成。 联接单元连接到平台的主体。
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Patent Agency Ranking26.发明授权영상 레이더 수신기의 디지털 영역에서의 잡음 톤 제거 방법, 이를 위한 영상 레이더 수신기 및 프로그램 기록매체 有权用于合成孔径雷达接收机，合成孔径雷达接收机的数字区域中的噪声消除方法和用于其方法的程序的计算机可读记录MIDI
公开(公告)号：KR101598719B1
公开(公告)日：2016-03-03
申请号：KR1020140173683
申请日：2014-12-05
Applicant: 한국항공우주연구원
CPC classification number: G01S13/90 , G01S7/023 , G01S7/2922 , G01S7/4021 , G01S2007/2883 , G01S2007/2886 , G01S7/40 , G01S13/89 , H04N5/21 , Y10S367/908
Abstract: 본발명은영상레이더수신기의디지털영역에서의잡음톤 제거방법, 이를위한영상레이더수신기및 프로그램기록매체에관한것이다. 본발명의일 실시예에따른디램핑구조를사용하는영상레이더수신기의디지털영역에서의잡음톤 제거방법은 (a)디램핑된영상신호의잡음톤 위치를추출하는과정과; (b)상기 (a)과정에의해추출된잡음톤 중에서제거할잡음톤을선택하는과정과; (c)상기 (b)과정에의해선택된잡음톤을원시데이터에서제거하는과정을포함하는것을특징으로한다.
Abstract translation: 本发明涉及一种去除合成孔径雷达接收机，合成孔径雷达接收机和其计算机可读记录介质的数字区域中的噪声音调的方法。 根据本发明的实施例，使用歪斜结构去除合成孔径雷达接收机的数字域中的噪声音调的方法包括：（a）提取增强图像信号的噪声音调位置的步骤; （b）选择由步骤（a）提取的要除去的噪声音的噪声音调的步骤; 以及（c）从原始数据中去除（b）步骤选择的噪声音调的步骤。
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公开(公告)号：KR101401120B1
公开(公告)日：2014-05-29
申请号：KR1020120155891
申请日：2012-12-28
Applicant: 한국항공우주연구원
CPC classification number: H04L25/085 , H04L25/025
Abstract: Provided is a signal processing device. The signal processing device includes an extraction unit for extracting a pilot signal from a received signal; a first prefilter for filtering the pilot signal by assuming the pilot signal as a signal related to an interference-limited environment; a second prefilter for filtering the pilot signal by assuming the pilot signal as a signal related to a noise-limited environment; and a determination unit for determining whether the first prefilter is applied to the received signal or whether the second prefilter is applied to the received signal by comparing output quality indexes of the first prefilter and the second prefilter.
Abstract translation: 提供了一种信号处理装置。 信号处理装置包括：提取单元，用于从接收信号中提取导频信号; 通过将导频信号作为与干扰限制环境相关的信号来对导频信号进行滤波的第一预滤波器; 通过将导频信号作为与噪声限制环境有关的信号来对导频信号进行滤波的第二预滤波器; 以及确定单元，用于通过比较第一预滤器和第二预滤器的输出质量指标，确定第一预滤波器是否被应用于接收信号，或者第二预滤波器是否被施加到接收信号。
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公开(公告)号：KR101388477B1
公开(公告)日：2014-04-23
申请号：KR1020120117949
申请日：2012-10-23
Applicant: 한국항공우주연구원
Abstract: 본 발명은 신호 처리 장치 및 방법에 관한 것으로, 이 장치는 센서로 인가되는 물리량을 누적 또는 적분하여 M-비트 디지털 값으로 출력하는 센서로부터 디지털 값을 입력받아 연이은 두 데이터 획득 시간에서의 물리량의 차이가 미리 정해진 범위 내에 있으면 디지털 카운터 증분의 절댓값이 2
M-1 보다 큰 경우 디지털 값의 증분을 센서가 측정한 물리량으로 계산한다.-
公开(公告)号：KR101145953B1
公开(公告)日：2012-05-15
申请号：KR1020090130848
申请日：2009-12-24
Applicant: 한국항공우주연구원
Abstract: 본 발명은 인공위성의 조립작업용 몸체패널을 용이하게 안전하게 전개하고 고정하기 위한 인공위성 몸체 패널의 전개 및 고정장치에 관한 것으로, 상기 장치는, 상기 몸체패널에 장착되는 스트롱 백; 고정편을 통해서 상기 몸체패널의 일측에 구비된 회전축에 장착되는 프레임; 상기 스트롱 백과 상기 프레임을 연결시켜주되 상기 스트롱 백의 높이 및 위치 간격이 보정될 수 있도록 하는 인터페이스 브라켓; 인공위성의 핸들링 포인트와 상기 프레임의 고정편에 결합되어서 상기 스트롱 백의 회전운동을 발생시키는 회전장치; 상기 고정부에 착설되어서 상기 몸체패널의 전개 이후에 회전 위치를 고정시켜주는 록킹 부재; 및 상기 몸체패널이 전개되었을 때 하향 처짐현상을 방지해주는 처짐방지 지지대를 포함하며, 인공위성 조립과정에서 빈번히 요구되는 몸체패널의 전개 및 장착을 보다 편리하고 안전하게 수행할 수 있게 하는 효과를 제공한다.
인공위성, 몸체패널, 스트롱 백, 핸들링 포인트, 인터페이스 브라켓-
公开(公告)号：KR1020110076159A
公开(公告)日：2011-07-06
申请号：KR1020090132791
申请日：2009-12-29
Applicant: 한국항공우주연구원
Abstract: PURPOSE: A mechanical ground support device is provided to transport, rotate and move an artificial satellite, to offer convenience and efficiency by performing various works using one structure, and to be structurally stable and simple against the load conditions added differently to an artificial satellite. CONSTITUTION: A mechanical ground support device comprises a movement support unit(110) attached to one side of an artificial satellite(10) and supporting the artificial satellite when moving the artificial satellite using a rope, a transportation support unit(120) supporting the movement support unit and functioning as a base when transporting the artificial satellite fixed to the movement support unit, and a rotation support unit(130) supported to the transportation support unit and attached to the other side of the artificial satellite to rotate the artificial satellite.
Abstract translation: 目的：提供一种用于运输，旋转和移动人造卫星的机械地面支撑装置，通过使用一种结构执行各种作品提供便利和效率，并且在结构上稳定和简单地抵抗与人造卫星不同的加载条件。 构成：机械地面支撑装置包括：移动支撑单元（110），其附接到人造卫星（10）的一侧并且在使用绳索移动人造卫星时支撑人造卫星;支撑运动的运输支撑单元（120） 支撑单元，并且当将固定在移动支撑单元上的人造卫星运送时作为基座起作用;以及旋转支撑单元，支撑在运输支撑单元上并附接到人造卫星的另一侧以旋转人造卫星。
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