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公开(公告)号：KR101315968B1
公开(公告)日：2013-10-08
申请号：KR1020110096442
申请日：2011-09-23
Applicant: 한국항공우주연구원
Abstract: 본 발명은 정보통신장치 및 그 제어방법에 관한 것으로, 본 발명에 따른 방법은 사용자 단말의 접근 및 이탈 여부 중 적어도 하나를 판단하는 단계, 그리고 사용자 단말이 접근 또는 이탈한 경우 사용자 단말에 대응하는 자동수행목록에 포함된 작업을 수행하는 단계를 포함한다. 본 발명에 따르면 반복적인 작업들을 자동으로 수행되도록 하여 사용자의 조작 실수를 줄이고 사용자 편의성을 증대시킬 수 있다. 또한 사용자가 급한 일로 자리를 비울 경우 수행되어야 하는 작업에 대해서도 자동 수행이 가능한바, 시스템의 안정적인 운영을 보장할 수 있다.
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公开(公告)号：KR1020090064740A
公开(公告)日：2009-06-22
申请号：KR1020070132049
申请日：2007-12-17
Applicant: 한국항공우주연구원
Abstract: An outer harness support of a satellite electrical test device and a support method using the same are provided to mount an outer harness on the satellite electrical test device safely by controlling a location and height of the outer harness support. An outer harness support(1) connected to a satellite electrical test device includes one member(11), the other member(12) and an attachable mount. One member includes a slit(111,112). The other member is vertically connected to one member. The attachable mount is adhered to an upper face(121) of the other member. Two slits are formed on one member.
Abstract translation: 提供卫星电气测试装置的外部线束支撑件和使用其的支撑方法，以通过控制外部线束支撑件的位置和高度来将外部线束安全地安装在卫星电气测试装置上。 连接到卫星电气测试装置的外部线束支撑件（1）包括一个构件（11），另一个构件（12）和可附接的支架。 一个构件包括狭缝（111,112）。 另一个成员垂直连接到一个成员。 可连接的安装件粘附到另一个构件的上表面（121）。 在一个构件上形成两个狭缝。
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公开(公告)号：KR1020090063643A
公开(公告)日：2009-06-18
申请号：KR1020070131090
申请日：2007-12-14
Applicant: 한국항공우주연구원
IPC: H01R13/633
Abstract: A connector separation device is provided to separate coupled connectors while uniform power is imposed thereon, thereby separating the connectors as minimizing damage to connector pins. A first plate and a second plate are arranged side by side in horizontal direction. Connection devices connect the first plate with the second plate, so that a distance between the first and second plates is changed. First pillars(21,25) are coupled with the first plate to rotate in place. Screw threads are formed in portions of the first pillars. Second pillars(29,33) are coupled with the second plate to rotate in place. Screw threads are formed in portions of the second pillars. A third plate is arranged in an upper part of the first plate in horizontal direction. A fourth plate is arranged in an upper part of the second plate in horizontal direction.
Abstract translation: 提供连接器分离装置以分离耦合的连接器，同时施加均匀的功率，从而将连接器分离成使对连接器引脚的损害最小化。 第一板和第二板在水平方向上并排布置。 连接装置将第一板与第二板连接，使得第一和第二板之间的距离改变。 第一支柱（21,25）与第一板联接以转动就位。 螺纹形成在第一柱的部分中。 第二柱（29,33）与第二板联接以转动就位。 螺纹形成在第二柱的部分中。 第三板在水平方向上布置在第一板的上部。 第四板在水平方向上布置在第二板的上部。
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公开(公告)号：KR1020090058606A
公开(公告)日：2009-06-10
申请号：KR1020070125229
申请日：2007-12-05
Applicant: 한국항공우주연구원
IPC: G05D1/08
CPC classification number: G05D1/0883
Abstract: An artificial satellite control signal verification apparatus and a method are provided to verify an electromagnetic filed signal and a valve control signal selectively by assembling a control signal verify device of an artificial satellite and the artificial satellite. An interface unit(520) supplies power to an artificial satellite from a power supply unit(510), and receives more than an electromagnetic filed signal and a valve signal from the artificial satellite body. A verification unit(530) processes more than one of the received electromagnetic filed signal and a valve signal, and verifies whether a normal condition of a posture control system or not through the received valve signal, and it also verify whether a normal condition of a solar panel through the received electromagnetic filed.
Abstract translation: 提供人造卫星控制信号验证装置和方法，通过组装人造卫星的控制信号验证装置和人造卫星来选择性地验证电磁场信号和阀门控制信号。 接口单元（520）从电源单元（510）向人造卫星供电，并且从人造卫星体接收多于电磁场信号和阀信号。 验证单元（530）处理接收到的电磁场信号和阀信号中的多于一个，并且通过接收到的阀信号来验证姿势控制系统的正常状态，并且还验证是否正常状态 太阳能电池板通过接收的电磁场。
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Patent Agency Ranking
公开(公告)号：KR100836191B1
公开(公告)日：2008-06-09
申请号：KR1020060132796
申请日：2006-12-22
Applicant: 한국항공우주연구원
CPC classification number: H04B17/364 , H04B7/185
Abstract: A loopback apparatus installed between electronic ground support equipment and a satellite for accurate telemetry is provided to enable electronic ground support equipment to measure the transmitting delay time of a ranging signal and a downlink carrier frequency difference accurately. A loopback apparatus(100) comprises an isolator(110), a circulator(120), a switching unit(130), and first and second attenuators(141,143). The isolator passes a signal outputted in electronic ground support equipment and blocks a signal inputted reversely. The circulator receives a signal outputted from the isolator through a first port and outputs the received signal to a second port, and outputs a signal inputted through the second port to a third port. The switching unit is selectively operated according to one of a first mode and a second mode. In the first mode, a signal transferred from the circulator is outputted to a satellite, and a signal transferred from the satellite is inputted to the electronic ground support equipment through the circulator. In the second mode, the signal outputted from the circulator is looped back to the electronic ground support equipment.
Abstract translation: 提供一种安装在电子地面支援设备和卫星之间用于精确遥测的环回装置，使得电子地面支援设备可以准确测量测距信号的发射延迟时间和下行载波频率差。 环回装置（100）包括隔离器（110），循环器（120），开关单元（130）以及第一和第二衰减器（141,143）。 隔离器通过在电子地面支持设备中输出的信号，并阻止反向输入的信号。 循环器通过第一端口接收从隔离器输出的信号，并将接收的信号输出到第二端口，并将通过第二端口输入的信号输出到第三端口。 根据第一模式和第二模式中的一种选择性地操作切换单元。 在第一模式中，将从循环器传送的信号输出到卫星，并且从卫星传送的信号通过循环器输入到电子地面支持设备。 在第二模式中，从循环器输出的信号环回到电子地面支撑设备。
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公开(公告)号：KR1020130032693A
公开(公告)日：2013-04-02
申请号：KR1020110096442
申请日：2011-09-23
Applicant: 한국항공우주연구원
CPC classification number: H04M1/7253 , G06F9/451 , G06F15/16 , G06F15/161 , H04B7/24 , H04W4/70
Abstract: PURPOSE: An information communication device and a control method thereof are provided to enhance the security of a system and to guarantee the stable management of the system by preventing a user from skipping a specific task. CONSTITUTION: When a user terminal approaches, a control unit(220) performs a task included in an automatic approach performance list corresponding to the user terminal. When the user terminal is separated, the control unit performs a task included in an automatic separation performance list corresponding to the user terminal. A communication unit(210) receives a wireless signal from the user terminal. If the intensity of the wireless signal is greater than the intensity of a set value, the control unit determines the approach of the user terminal. If the intensity of the wireless signal is less than the intensity of the set value, the control unit determines the separation of the user terminal. [Reference numerals] (200) Information communication device; (210) Communication unit; (220) Control unit; (230) Storage unit;
Abstract translation: 目的：提供一种信息通信装置及其控制方法，以增强系统的安全性，并通过防止用户跳过特定任务来保证系统的稳定管理。 构成：当用户终端接近时，控制单元（220）执行包括在与用户终端对应的自动进场表现列表中的任务。 当用户终端分离时，控制单元执行包括在与用户终端对应的自动分离表现列表中的任务。 通信单元（210）从用户终端接收无线信号。 如果无线信号的强度大于设定值的强度，则控制单元确定用户终端的接近。 如果无线信号的强度小于设定值的强度，则控制单元确定用户终端的分离。 （附图标记）（200）信息通信装置; （210）通讯单元; （220）控制单元; （230）存储单元;
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公开(公告)号：KR101165286B1
公开(公告)日：2012-07-19
申请号：KR1020110047784
申请日：2011-05-20
Applicant: 한국항공우주연구원
Abstract: PURPOSE: A GPS(Global Positioning System) base mobile type time synchronizing apparatus and method are provided to synchronize time of a device which is driven within an independent closed network by using GPS standard time. CONSTITUTION: A mobile type time synchronizing apparatus comprises a GPS signal receiver(210), a controller(230), and a communication unit(250). The GPS signal receiver receives a GPS signal. The controller calculates GPS standard time from the GPS signal and establishes standard time. The communications unit transfers a time synchronization signal created based on the established standard time to a device which is connected with direct communications. The device is driven within a closed network or is connected to other devices with direct communications.
Abstract translation: 目的：提供GPS（全球定位系统）基地移动式时间同步装置和方法，以通过使用GPS标准时间来同步在独立封闭网络内驱动的设备的时间。 构成：移动式时间同步装置包括GPS信号接收器（210），控制器（230）和通信单元（250）。 GPS信号接收机接收GPS信号。 控制器根据GPS信号计算GPS标准时间并建立标准时间。 通信单元将基于建立的标准时间创建的时间同步信号传送到与直接通信相连接的设备。 该设备在封闭的网络内驱动，或连接到具有直接通信的其他设备。
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公开(公告)号：KR100945686B1
公开(公告)日：2010-03-05
申请号：KR1020070131090
申请日：2007-12-14
Applicant: 한국항공우주연구원
IPC: H01R13/633
Abstract: 본 발명은 체결된 커넥터를 서로 분리하기 위한 커넥터 분리 장치에 관한 것이다. 커넥터 분리 장치는 수평방향으로 나란하게 배열되는 제1 플레이트와 제2 플레이트, 상기 제1 플레이트와 상기 제2 플레이트 사이의 거리가 변경될 수 있도록 상기 제1 플레이트와 상기 제2 플레이트를 연결하는 하나 이상의 연결기구, 제자리에서 회전 가능하도록 상기 제1 플레이트에 체결되며 일부에 나사 산이 형성되어 있는 하나 이상의 제1 기둥, 제자리에서 회전 가능하도록 상기 제2 플레이트에 체결되며 일부에 나사 산이 형성되어 있는 하나 이상의 제2 기둥, 상기 제1 플레이트의 상부에 수평방향으로 배치되며 상기 제1 기둥의 회전에 대응하여 상하 방향으로 이동할 수 있도록 상기 제1 기둥의 나사 산에 나사 결합되는 제3 플레이트, 상기 제2 플레이트의 상부에 수평방향으로 배치되며 상기 제2 기둥의 회전에 대응하여 상하 방향으로 이동할 수 있도록 상기 제2 기둥의 나사 산에 나사 결합되는 제4 플레이트, 그리고 상기 제3 플레이트와 상기 제4 플레이트가 상하 이동될 수 있도록 상기 제1 기둥과 상기 제2 기둥을 회전시키는 구동 유닛을 포함한다. 커넥터 분리 장치에 의해 커넥터 핀의 손상 없이 체결된 커넥터가 분리될 수 있다.
커넥터, 커넥터 핀, 분리, 나사 산-
公开(公告)号：KR100791322B1
公开(公告)日：2008-01-04
申请号：KR1020060130683
申请日：2006-12-20
Applicant: 한국항공우주연구원
IPC: G01M99/00
Abstract: A control apparatus with an interlock function for each satellite function test is provided to prevent function tests which give a serious impact on a satellite and ground supporting equipment from being performed simultaneously. A control apparatus(200) with an interlock function includes first to fifth relays. The first relay connects a first DC power of ground supporting equipment(100) to a main bus(310) of a satellite(300) through a predetermined diode. The second relay connects the first DC power directly to the main bus of the satellite. The third relay connects a battery(320) of the satellite to the main bus of the satellite. The fourth relay connects a second DC power of the ground supporting equipment to the battery of the satellite. The fifth relay connects a DC electric load of the ground supporting equipment to the battery of the satellite. Therefore, the control apparatus controls the connection between the ground supporting equipment and the satellite.
Abstract translation: 提供具有每个卫星功能测试的互锁功能的控制装置，以防止对卫星和地面支持设备的同时执行造成严重影响的功能测试。 具有互锁功能的控制装置（200）包括第一至第五继电器。 第一继电器通过预定二极管将地面支撑设备（100）的第一DC电力连接到卫星（300）的主总线（310）。 第二个继电器将第一直流电源直接连接到卫星的主总线。 第三继电器将卫星的电池（320）连接到卫星的主总线。 第四个继电器将地面支撑设备的第二直流电源连接到卫星的电池。 第五个继电器将地面支持设备的直流电负载连接到卫星的电池。 因此，控制装置控制地面支撑设备与卫星之间的连接。
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