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1. 发明公开

KR1020100131088A 위성체 배터리 모사장치 有权
标题翻译：卫星电池模拟器
公开(公告)号：KR1020100131088A
公开(公告)日：2010-12-15
申请号：KR1020090049791
申请日：2009-06-05
申请人： 한국항공우주연구원
发明人： 박병하 , 최종연 , 조승원 , 김관용
IPC分类号： H01M10/48 , B64G1/66
CPC分类号： H01M10/4285 , B64G1/66 , H01M10/48 , Y02E60/12
摘要： PURPOSE: A satellite battery simulator is provided to test the performance of a satellite wattmeter for reducing the testing cost, and to remove errors form the satellite wattmeter. CONSTITUTION: A satellite battery simulator(200) comprises the following: a power storage unit(220) including a battery(130) for testing a satellite; a power supplying unit(230) supplying electricity to the power storage unit for charging the battery; a battery interface(240) supplying the power from the power storage unit to a satellite wattmeter; and a controller(210) controlling the power source route.
摘要翻译：目的：提供卫星电池模拟器，用于测试卫星功率表的性能，以降低测试成本，并消除卫星瓦特计的误差。构成：卫星电池模拟器（200）包括以下部件：包括用于测试卫星的电池（130）的蓄电单元（220）供电单元，向所述蓄电单元供电以对所述电池充电; 电池接口（240），其将来自所述蓄电单元的电力提供给卫星瓦特计; 以及控制电源路径的控制器（210）。

2. 发明授权

KR100791322B1 위성체 기능 시험 별 인터록 기능을 구비한 제어장치 失效
标题翻译：具有互锁功能的控制装置
公开(公告)号：KR100791322B1
公开(公告)日：2008-01-04
申请号：KR1020060130683
申请日：2006-12-20
申请人： 한국항공우주연구원
发明人： 박병하 , 최종연 , 권재욱 , 윤영수 , 조승원
IPC分类号： G01M99/00
摘要： 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.
摘要翻译：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。

3. 发明授权

KR101086752B1 위성체 배터리 모사장치 有权
标题翻译：卫星电池模拟器
公开(公告)号：KR101086752B1
公开(公告)日：2011-11-24
申请号：KR1020090049791
申请日：2009-06-05
申请人： 한국항공우주연구원
发明人： 박병하 , 최종연 , 조승원 , 김관용
IPC分类号： H01M10/48 , B64G1/66
摘要： 본 발명은 위성체 배터리 모사장치에 관한 것이다. 본 발명에 따른 장치는 위성체 배터리와 동일한 규격의 위성체 시험용 배터리를 포함하는 전원 저장부, 전원 저장부에 전력을 공급하여 위성체 시험용 배터리를 충전시키거나 위성 전력계에 전력을 공급하는 전원 공급부, 전원 공급부 또는 전원 저장부로부터 제공되는 전력을 전원 경로에 따라 위성 전력계에 공급하는 배터리 인터페이스, 그리고 전원 경로를 제어하는 제어부를 포함한다. 본 발명에 의하면, 고가의 장비인 위성체 배터리 대신 위성체 배터리 모사장치를 이용하여 위성 전력계의 성능을 검증함으로써 검증 시 소요되는 비용을 줄일 수 있다. 또한 위성 전력계의 성능 검증을 통해 에러를 찾아 제거함으로써, 위성체의 실제 구동 시 발생할 에러를 미연에 방지할 수 있고 위성체의 안정성 및 신뢰성을 증가시킬 수 있다.
위성체, 배터리, 모의실험, 시뮬레이터, 모사장치

4. 发明授权

KR100802380B1 위성체 배터리의 제어 장치 失效
标题翻译：用于控制卫星电池的装置
公开(公告)号：KR100802380B1
公开(公告)日：2008-02-13
申请号：KR1020060119597
申请日：2006-11-30
申请人： 한국항공우주연구원
发明人： 박병하 , 최종연 , 권재욱 , 윤영수 , 조승원
IPC分类号： H02J9/04 , H02J9/06
摘要： An apparatus for controlling a satellite battery is provided to stably block power supplied from the satellite battery to a satellite power supply system regardless of an error of an uninterruptible power supply or a power control device. An apparatus for controlling a satellite battery(200) supplies power to a satellite power supply system and includes a battery control part(210) and a satellite battery protection unit(220). The battery control part is placed between the satellite power supply system and the satellite battery and has a battery blocking relay(215). The battery blocking relay controls supply of satellite battery power to the satellite power supply system. The battery protection part operates the battery blocking relay to block connection between the satellite battery and the satellite power supply system by using the satellite battery power during occurrence of an error of an outer power control device to control operation of the battery blocking relay.
摘要翻译：提供一种用于控制卫星电池的装置，用于稳定地阻止从卫星电池提供给卫星电源系统的电力，而不管不间断电源或电源控制装置的错误。一种用于控制卫星电池（200）的设备向卫星电源系统供电并且包括电池控制部分（210）和卫星电池保护单元（220）。电池控制部分放置在卫星电源系统和卫星电池之间，并具有电池阻塞继电器（215）。电池阻塞继电器控制卫星电源系统的卫星电池供电。电池保护部分操作电池阻塞继电器，以在发生外部电力控制装置的错误期间使用卫星电池电力来阻止卫星电池和卫星电源系统之间的连接，以控制电池阻塞继电器的操作。

5. 发明公开

KR1020090058606A 인공 위성의 제어 신호 검증 장치 및 방법 无效
标题翻译：人造卫星控制信号验证装置和方法
公开(公告)号：KR1020090058606A
公开(公告)日：2009-06-10
申请号：KR1020070125229
申请日：2007-12-05
申请人： 한국항공우주연구원
发明人： 박병하 , 최종연 , 권재욱 , 윤영수 , 조승원 , 김영윤
IPC分类号： G05D1/08
CPC分类号： G05D1/0883
摘要： 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.
摘要翻译：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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