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1. 发明授权

KR101363226B1 위성항법메시지의 고장 검출 향상을 위한 기준국 안테나 배치 방법 및 위성항법메시지의 고장 검출 장치 有权
标题翻译：采用基站天线改善全球导航卫星信息故障检测方法和检测全球导航卫星信息故障的方法
公开(公告)号：KR101363226B1
公开(公告)日：2014-02-14
申请号：KR1020120122861
申请日：2012-11-01
申请人： 건국대학교 산학협력단 , 한국항공우주연구원
发明人： 이영재 , 남기욱 , 성상경 , 윤영선 , 안종선 , 원대희
IPC分类号： G01S19/20 , G01S19/23
摘要： The present invention relates to a method for deploying a base station antenna to improve fault detection of a global navigation satellite message and a fault detection apparatus of the global navigation satellite message. The method for deploying a base station antenna to improve fault detection of a global navigation satellite message received from a satellite of the present invention includes: an apex coordinate calculation step of calculating each apex coordinate of a polygon corresponding to the number of a plurality of base station antennas; and an antenna deployment step of deploying each of the plurality of base station antennas at each calculated apex coordinate of the polygon in order to generate a base line among the plurality of base station antennas, by moving one base station antenna among the plurality of deployed base station antennas to generate an additional base line which is independent of the generated base line. [Reference numerals] (121) Receiver A; (122) Receiver B; (123) Receiver C; (124) Receiver D
摘要翻译：本发明涉及一种用于部署基站天线以改善全球导航卫星消息的故障检测和全球导航卫星消息的故障检测装置的方法。用于部署基站天线以改善从本发明的卫星接收的全球导航卫星消息的故障检测的方法包括：顶点坐标计算步骤，计算与多个基站的数量对应的多边形的每个顶点坐标站天线; 以及天线部署步骤，通过在多个基站天线之间移动一个基站天线，将多个基站天线中的每一个部署在多边形的每个计算出的顶点坐标处，以便生成多个基站天线之间的基准线以产生独立于所生成的基线的附加基线。（附图标记）（121）接收器A; （122）接收器B; （123）接收者C; （124）接收者D

2. 发明公开

KR1020170078065A 보호 수준 결정 시스템 및 그 방법 有权
公开(公告)号：KR1020170078065A
公开(公告)日：2017-07-07
申请号：KR1020150188192
申请日：2015-12-29
申请人： 한국항공우주연구원
发明人： 윤영선 , 이은성 , 허문범 , 남기욱
IPC分类号： G01S19/23 , G01S19/08
CPC分类号： G01S19/08 , G01S19/20
摘要： 본발명의일실시예에따른보호수준결정시스템이개시된다. 상기보호수준결정시스템은위성궤도및 시계오차에대한보정오차, 전리층오차에대한보정오차, 위성에대한수신기잡음과다중경로보정오차, 대류층보정오차및 위치항법신호를수신하는수신부, 상기위성궤도및 시계오차에대한보정오차및 상기전리층오차에대한보정오차에적용하는제1 조정계수를산출하는제1 산출부, 및상기제1 조정계수를적용하여보호수준을산출하는제2 산출부를포함한다.

3. 发明授权

KR101446427B1 고장 검출 임계값 갱신 장치 및 방법 有权
标题翻译：自动更新故障检测手段的装置和方法
公开(公告)号：KR101446427B1
公开(公告)日：2014-10-06
申请号：KR1020130045975
申请日：2013-04-25
申请人： 한국항공우주연구원
发明人： 윤영선 , 조정호 , 남기욱 , 허문범
IPC分类号： G01S19/23 , G01S19/20 , G01S19/40
摘要： An apparatus for updating fault detection thresholds is provided. The apparatus for updating the fault detection thresholds comprises: an environmental change detector for detecting a change in the signal reception environment; a controller for calculating a value of an environment change indicator based on the results of the reception environment of a detection signal and for requesting the update of a detection threshold which indicates whether correction information has a failure by determining a change in the reception environment of the signal; and a detection threshold updating unit for updating the detection threshold in response to the request.
摘要翻译：提供了一种用于更新故障检测阈值的装置。用于更新故障检测阈值的装置包括：环境变化检测器，用于检测信号接收环境的变化; 控制器，用于基于检测信号的接收环境的结果来计算环境变化指示符的值，并且通过确定修正信息的接收环境的变化来请求更新指示校正信息是否具有故障的检测阈值信号; 以及检测阈值更新单元，用于响应于该请求来更新检测阈值。

4. 发明授权

KR101151670B1 기준국 수신기 시계오차 조정 효과를 고려한 ＧΝＳＳ 의사거리 보정치 표준편차 설정방법 有权
标题翻译：考虑到参考接收机时钟调整效果的GNSS精密校正的标准偏差建立方法
公开(公告)号：KR101151670B1
公开(公告)日：2012-06-08
申请号：KR1020110134274
申请日：2011-12-14
申请人： 한국항공우주연구원
发明人： 윤영선 , 조정호 , 허문범 , 남기욱
IPC分类号： G01S19/39 , G08G5/00
摘要： PURPOSE: A standard deviation setting method of a global navigation satellite system(GNSS) pseudo range correction value is provided to accurately estimate a user location error level and performance of an integrity monitoring algorithm. CONSTITUTION: The location of a navigation satellite is calculated from a received signal from each navigation satellite. An elevation angle of each navigation satellite is acquired based on the location of a receiver(S100). A standard deviation of a pseudo range correction value according to the elevation angle is calculated using a navigation signal measurement value collected from each navigation satellite(S200). A standard deviation which considers view error control effects is created from the standard deviation of the pseudo range correction value and the elevation angle with respect to the navigation satellite(S300). The standard deviation which considers the view error control effects with respect to the navigation satellite is inputted as an input value of an integrity monitoring algorithm(S400). A broadcasting message receives the standard deviation of the pseudo range correction value(S500).
摘要翻译：目的：提供全球导航卫星系统（GNSS）伪距校正值的标准偏差设置方法，以准确估计用户位置误差水平和完整性监测算法的性能。构成：根据每个导航卫星的接收信号计算导航卫星的位置。基于接收机的位置获取每个导航卫星的仰角（S100）。使用从每个导航卫星收集的导航信号测量值来计算根据仰角的伪距校正值的标准偏差（S200）。考虑视差误差控制效果的标准偏差是根据伪距校正值的标准偏差和相对于导航卫星的仰角产生的（S300）。作为完整性监视算法的输入值，输入考虑到对导航卫星的视差误差控制效果的标准偏差（S400）。广播消息接收伪距校正值的标准偏差（S500）。

5. 发明授权

KR102030737B1 안전 항로 설계 장치 및 방법 有权
公开(公告)号：KR102030737B1
公开(公告)日：2019-10-10
申请号：KR1020180067855
申请日：2018-06-14
申请人： 한국항공우주연구원
发明人： 김희성 , 윤영선 , 강희원 , 이은성 , 윤상은
IPC分类号： G01C21/20 , B64C39/02 , G01S19/38

6. 发明授权

KR101761782B1 보호 수준 결정 시스템 및 그 방법 有权
标题翻译：保护等级确定系统和方法
公开(公告)号：KR101761782B1
公开(公告)日：2017-07-26
申请号：KR1020150188192
申请日：2015-12-29
申请人： 한국항공우주연구원
发明人： 윤영선 , 이은성 , 허문범 , 남기욱
IPC分类号： G01S19/23 , G01S19/08
CPC分类号： G01S19/08 , G01S19/20
摘要： 본발명의일실시예에따른보호수준결정시스템이개시된다. 상기보호수준결정시스템은위성궤도및 시계오차에대한보정오차, 전리층오차에대한보정오차, 위성에대한수신기잡음과다중경로보정오차, 대류층보정오차및 위치항법신호를수신하는수신부, 상기위성궤도및 시계오차에대한보정오차및 상기전리층오차에대한보정오차에적용하는제1 조정계수를산출하는제1 산출부, 및상기제1 조정계수를적용하여보호수준을산출하는제2 산출부를포함한다.
摘要翻译：公开了根据本发明实施例的保护等级确定系统。用于确定卫星轨道和时钟误差的校正误差，在电离层误差的校正误差，用于接收接收机噪声和多径的校正误差，对流区校正误差和位置的导航信号的卫星，卫星的轨道上的接收机保护系统和和校正时钟误差的误差包括用于计算第一计算单元的第二计算器，和保护通过应用第一调整系数用于计算第一调整系数应用于所述校正错误的电离层误差的电平。

7. 发明授权

KR101240629B1 ＡＤＳ-Ｂ 시스템이 탑재된 항공기를 이용한 미지신호 검출 및 발생원 위치 추정방법 有权
标题翻译：使用飞机与ADS-B系统的未知信号的检测和本地化方法
公开(公告)号：KR101240629B1
公开(公告)日：2013-03-11
申请号：KR1020120137566
申请日：2012-11-30
申请人： 한국항공우주연구원
发明人： 윤영선 , 조정호 , 허문범 , 남기욱
IPC分类号： G01S19/02 , G01S19/39 , G01S19/14
CPC分类号： G01S19/46 , G01S5/0036 , G01S5/0072 , G01S5/02 , G01S5/0205 , G01S5/0221 , G01S5/04 , G01S5/06 , G01S19/03 , G01S19/21
摘要： PURPOSE: A method for detecting the location of an unknown signal a generation source using an aircraft where an ADS-B(Automatic Dependent Surveillance-Broadcast) system is mounted is provided to quickly and accurately detect the location of unknown signals and a generation source by excluding the influence of signal diffraction or reflection. CONSTITUTION: Multiple aircrafts in flight where an ADS-B system is mounted receive GNSS(Global Navigation Satellite System) signals, transmitted from navigation satellites and a generation source of unknown signals, and the unknown signals, and transmit the received signals to an air traffic control center through the ADS-B system(S100). The air traffic control center detects whether unknown signals are included in the received signals by using either TDOA(Time Difference Of Arrival) technique, TOA(Time Of Arrival) technique, or AOA(Angel Of Arrival) technique(S200). If unknown signals are included, the generation source location of the unknown signals is estimated by using either TDOA(Time Difference Of Arrival) technique, TOA(Time Of Arrival) technique, or AOA(Angel Of Arrival) technique(S300). The estimated information about the unknown signals and the generation source location of the unknown signals is transmitted from ADS-B ground equipment to nearby aircrafts and the air traffic control center through the FIS-B(Flight Information Services-Broadcast) or NOTAM(Notice To Airmen)(S400). [Reference numerals] (S100) Signal obtaining step; (S200) Unknown signal detecting step; (S300) Unknown signal generation source location estimating step; (S400) Unknown signal generation information transmitting step
摘要翻译：目的：提供一种使用安装ADS-B（自动相关监控广播）系统的飞机检测未知信号位置的方法，用于快速准确地检测未知信号和发生源的位置，排除信号衍射或反射的影响。构成：安装ADS-B系统的飞行中的多架飞机接收从导航卫星和未知信号发生源发射的GNSS（全球导航卫星系统）信号和未知信号，并将接收到的信号发送到空中交通控制中心通过ADS-B系统（S100）。空中交通管制中心通过使用TDOA（到达时差）技术，TOA（到达时间）技术或AOA（到达天使）技术（S200）来检测接收到的信号中是否包含未知信号。如果包括未知信号，则使用TDOA（到达时差）技术，TOA（到达时间）技术或AOA（到达天使）技术（S300）来估计未知信号的生成源位置。关于未知信号的估计信息和未知信号的发生源位置通过FIS-B（飞行信息服务广播）或NOTAM（注意事项）从ADS-B地面设备传输到附近的飞机和空中交通管制中心空军）（S400）。（附图标记）（S100）信号获取步骤; （S200）未知信号检测步骤; （S300）未知信号发生源位置估计步骤; （S400）未知信号生成信息发送步骤

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