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公开(公告)号：KR101745605B1
公开(公告)日：2017-06-09
申请号：KR1020160172879
申请日：2016-12-16
Applicant: 한국항공우주연구원
CPC classification number: Y02A90/18 , G01S13/951 , G01S19/20 , G01W1/00
Abstract: 본발명의일 실시예는이온층측정포인트에서의이온층측정결과로부터이온층의상태를모델링하는프로세서를이용하여이온층을감시하는방법에있어서, 상기프로세서의수신부를통하여, 상기이온층측정포인트에서복수개의이온층투과포인트들각각에대한이온층투과지연시간오차측정값을수신하는단계; 상기프로세서의제어부를통하여, 상기복수개의이온층투과포인트들에대하여두 개이상의모델링식들중 어떤모델링식을사용할수 있는지검사하는단계; 상기제어부를통하여, 상기검사결과를기초로상기이온층측정포인트에서이온층의상태를모델링하기위하여사용할모델링식을결정하는단계; 및상기제어부를통하여, 상기결정한모델링식에상기이온층투과지연시간오차측정값을대입하여이온층의상태를모델링하는단계;를포함하는, 이온층감시방법을개시한다.
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公开(公告)号：KR101742747B1
公开(公告)日：2017-06-01
申请号：KR1020160164395
申请日：2016-12-05
Applicant: 한국항공우주연구원
Abstract: 본발명의일 실시예에따른위성항법장치의운용방법은, 하나이상의위성(Satellite)으로부터제1 신호를수신하여상기위성항법장치의현재위치를산출하는위치산출단계; 하나이상의외부장치로부터수신된제2 신호및 상기위성항법장치의현재상태에대응되는제3 신호중 적어도하나에기초하여상기위성항법장치의동작모드(Mode)를결정하는동작모드결정단계; 및상기동작모드가제1 모드인경우상기산출된위치에대한정보를포함하는제4 신호를상기외부장치로전송하는신호전송단계;를포함할수 있다.
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公开(公告)号：KR101693304B1
公开(公告)日：2017-01-06
申请号：KR1020150161563
申请日：2015-11-18
Applicant: 한국항공우주연구원
Abstract: 본발명에의한정밀위치결정장치는제1광대역신호모듈(110) 및 GPS수신기(120)가부착되고, 상공을비행하는복수의무인기(100) 및미리정해진위치에구비되어상기제1광대역신호모듈(110)과의통신으로스스로의위치를결정하는단말기(200)를포함하여이루어지는것을특징으로한다. 또한본 발명에의한정밀위치결정장치를이용한임야에서의정밀위치결정방법은각각의상기 GPS수신기(120)가인공위성(300)으로부터 GPS신호를수신하여상기복수의무인기(100) 각각의위치를파악하는무인기위치파악단계(S1), 상기복수의무인기(100) 각각에구비된상기제1광대역신호모듈(110)이상기단말기(200)와통신하여상기무인기(100)의위치및 상기무인기(100)와단말기(200)의거리를상기단말기(200)로송신하는위치정보송신단계(S2) 및상기제1광대역신호모듈(110)로부터수신한정보를이용하여상기단말기(200)의위치를결정하는단말기위치파악단계(S3)를포함하여이루어지는것을특징으로한다.
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公开(公告)号：KR101672710B1
公开(公告)日：2016-11-16
申请号：KR1020150175593
申请日：2015-12-10
Applicant: 한국항공우주연구원
Abstract: 상술한목적을달성하기위한본 발명에따른증강현실을이용한실내위치모니터링시스템은실내에설치되어실내에진입한내부요원의위치를결정하기위한신호를송신하는복수의실내송신기; 실내요원이착용하고전파측위기반, 추측항법기반, 또는전파측위와추측항법을통합하여실내요원의위치를결정하는내부요원장비; 실외에설치되어실외에서실내요원을모니텅링하기위한관측요원의위치를결정하기위한신호를송신하는복수의실외송신기; 관측요원이착용하고실외송신기의설치된위치정보와거리측정이가능한무선신호를수신하여상기관측요원의위치를결정하는관측요원장비; 내부요원장비와관측요원장비로부터각각실내요원위치정보와관측요원위치정보수신하여, 상대위치를결정하고관측요원의시선벡터를계산하여관측요원장비에증강현실로디스플레이될수 있는영상을생성하는중앙처리서버;를포함하여, 화재및 붕괴사고등의현장에서구조활동전개시, 실내에위치한구조요원의위치정보를제공함으로써, 효율적인구조활동전개는물론구조요원의안전을확보할수 있는효과가있다.
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公开(公告)号：KR101446427B1
公开(公告)日：2014-10-06
申请号：KR1020130045975
申请日：2013-04-25
Applicant: 한국항공우주연구원
Abstract: 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.
Abstract translation: 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。
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Patent Agency Ranking
公开(公告)号：KR101445723B1
公开(公告)日：2014-10-01
申请号：KR1020130142682
申请日：2013-11-22
Applicant: 한국항공우주연구원
IPC: G08C15/00
CPC classification number: G08C15/06
Abstract: The present invention discloses a long distance system capable of performing time synchronization with high precision at the minimum cost by transmitting/receiving a time synchronization signal using one of a power line and a communications line that are commonly installed and used between sub-systems constituting a predetermined long distance system, and a time synchronization method performed in the long distance system. The long distance system includes a control sub-system and a plurality of sub-systems. The control sub-system includes a control unit, an atomic clock, and a synchronization generator. The control unit corrects the time of the atomic clock using satellite navigation signals received through a satellite navigation, and the synchronization generator generates a time synchronization signal using time corrected of the atomic clock. Each of the sub-systems includes a time synchronization terminal that is connected with the control sub-system through at least one of the power line and the communications line and performs time synchronization using the time synchronization signal received through one of the power line and the communications line.
Abstract translation: 本发明公开了一种长距离系统，其能够以最小成本以高精度进行时间同步，通过使用在构成一个或多个子系统的子系统之间通常安装和使用的电力线和通信线路之一来发送/接收时间同步信号 预定长距离系统，以及在长距离系统中执行的时间同步方法。 长距离系统包括控制子系统和多个子系统。 控制子系统包括控制单元，原子钟和同步发生器。 控制单元使用通过卫星导航接收到的卫星导航信号来校正原子钟的时间，同步发生器使用原子钟校正的时间产生时间同步信号。 每个子系统包括时间同步终端，其通过电力线和通信线路中的至少一个与控制子系统连接，并使用通过电力线和通信线路中的一个接收的时间同步信号来执行时间同步 通信线路。
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公开(公告)号：KR101436265B1
公开(公告)日：2014-09-22
申请号：KR1020130151238
申请日：2013-12-06
Applicant: 한국항공우주연구원
Abstract: A dynamic state compensation system may include a speed detection unit which detects the speed of a first moving object; and a communications unit which transmits the location data of the dynamic state compensation system and the detected speed of the first moving object to the first moving object. Also, a positioning device which receives data from the dynamic state compensation system includes a GPS module which determines at least one among the location data and the speed data of the positioning device; and a communications unit which receives the location data of the dynamic state compensation system and the detected speed data of the positioning device from the dynamic state compensation system. The GPS module can compensate at least one among the location data and the speed data of the positioning device based on the location data of the dynamic state compensation system and the detected speed data of the positioning device received in the communications unit.
Abstract translation: 动态状态补偿系统可以包括速度检测单元，其检测第一移动物体的速度; 以及通信单元，其将动态状态补偿系统的位置数据和检测到的第一移动对象的速度发送到第一移动对象。 此外，从动态状态补偿系统接收数据的定位装置包括GPS模块，其确定定位装置的位置数据和速度数据中的至少一个; 以及通信单元，其从动态状态补偿系统接收动态状态补偿系统的位置数据和检测到的定位装置的速度数据。 GPS模块可以基于动态状态补偿系统的位置数据和在通信单元中接收的定位装置的检测速度数据，来补偿定位装置的位置数据和速度数据中的至少一个。
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公开(公告)号：KR101271006B1
公开(公告)日：2013-06-04
申请号：KR1020120139240
申请日：2012-12-03
Applicant: 한국항공우주연구원
IPC: H04L12/861 , H04L29/06
CPC classification number: H04L47/629 , H04L47/2416 , H04L47/27 , H04L47/6275 , H04L69/163
Abstract: PURPOSE: A transmission method of GNSS(Global navigation satellite system) data for real time processing is provided to design a data format and a transmission priority determination method for real-time data transmission through a commercial wired network, thereby minimizing delay time in data processing and immediately delivering correction data to users. CONSTITUTION: A transmission method of GNSS data comprises the steps of: acquiring basic data by each base station(S100); and transmitting the basic data to a central station(S200). The basic data includes GNSS data which is transmitted from a plurality of GPSs; weather data which is acquired by each base station and the location data of each base station. The format of the data transmitted to the central station is organized with a preamble which indicates a beginning of a data packet, a time stamp, a receiving station ID which is identification of a base station, a packet ID, packet message data, an acquire data time which indicates the time when the base station acquired data, weather data, and a receiving station health flag which indicates whether the base station operates normally or not. The central station receives the data received according to the priority determined by a weighted fair queuing algorithm. [Reference numerals] (S100) Basic data acquisition step; (S200) Data transmission step
Abstract translation: 目的：提供一种用于实时处理的GNSS（全球导航卫星系统）数据传输方法，用于设计通过商业有线网络进行实时数据传输的数据格式和传输优先级确定方法，从而最大限度地减少数据处理中的延迟时间 并立即向用户发送校正数据。 构成：GNSS数据的传输方法包括以下步骤：获取每个基站的基本数据（S100）; 以及将基本数据发送到中心站（S200）。 基本数据包括从多个GPS发送的GNSS数据; 每个基站获取的天气数据和每个基站的位置数据。 发送到中心站的数据的格式由表示数据分组的开始的前导码，时间戳，作为基站的识别的接收站ID，分组ID，分组消息数据，获取 指示基站获取数据的时间的数据时间，天气数据和指示基站是否正常操作的接收站健康标志。 中央站根据由加权公平排队算法确定的优先级接收接收到的数据。 （附图标记）（S100）基本数据获取步骤; （S200）数据发送步骤
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公开(公告)号：KR101227911B1
公开(公告)日：2013-02-15
申请号：KR1020120157441
申请日：2012-12-28
Applicant: 한국항공우주연구원
IPC: G01S19/01
Abstract: PURPOSE: A simulated signal generating system for disturbance signal generation source position tracking is provided to perform a simulated experiment for tracking the position of a disturbance signal generation source in an environment close to the real situation. CONSTITUTION: A simulated signal generating system for disturbance signal generation is as follows. Disturbance signal simulator controller(10) generates the positional information of a satellite navigation receiver(2) and the positional information of the disturbance signal generation source in real-time. Satellite navigation signal simulator(1) inputs the positional information of the satellite navigation receiver generated from a disturbance signal simulator controller(10), and generates the satellite navigation signal depending on the positional information of the satellite navigation receiver. A disturbance signal generation controller(20) calculates the frequency change, the attenuation ratio and the phase delay respectively using the positional information of the satellite navigation receiver generated from the satellite navigation disturbance signal simulator controller and disturbance signal generating source. A signal generator(30) generates the disturbing signal using the frequency change, the attenuation ratio and the phase delay calculated from the disturbing signal generation controller. A signal coupler(40) generates the satellite navigation signal including the disturbance signal by coupling the satellite navigation signal transmitted from the satellite navigation signal simulator and the disturbance signal transmitted from the signal generator. Satellite navigation signal receives the satellite navigation signal including the disturbance signal generated from the signal coupler. [Reference numerals] (10) Satellite navigation disturbance signal simulator controller; (20) Disturbance signal generation controller; (A1) Satellite navigation signal simulator 1; (A2) Satellite navigation signal simulator n; (B1) Signal generator 1; (B2) Signal generator n; (C1) Signal coupler 1; (C2) Signal coupler n; (D1) Satellite navigation receiver 1; (D2) Satellite navigation receiver n
Abstract translation: 目的：提供一种用于干扰信号发生源位置跟踪的模拟信号发生系统，用于在接近实际环境的环境中跟踪扰动信号发生源的位置进行仿真实验。 构成：用于产生干扰信号的模拟信号发生系统如下。 干扰信号模拟器控制器（10）实时地产生卫星导航接收机（2）的位置信息和干扰信号发生源的位置信息。 卫星导航信号模拟器（1）输入从干扰信号模拟器控制器（10）产生的卫星导航接收机的位置信息，并根据卫星导航接收机的位置信息产生卫星导航信号。 干扰信号发生控制器（20）分别使用从卫星导航干扰信号模拟器控制器和干扰信号发生源产生的卫星导航接收机的位置信息来分别计算频率变化，衰减比和相位延迟。 信号发生器（30）使用从干扰信号发生控制器计算的频率变化，衰减比和相位延迟来产生干扰信号。 信号耦合器（40）通过耦合从卫星导航信号模拟器发送的卫星导航信号和从信号发生器发送的干扰信号，产生包括干扰信号的卫星导航信号。 卫星导航信号接收包括从信号耦合器产生的干扰信号的卫星导航信号。 [参考数字]（10）卫星导航扰动信号模拟器控制器; （20）干扰信号发生控制器; （A1）卫星导航信号模拟器1; （A2）卫星导航信号模拟器n; （B1）信号发生器1; （B2）信号发生器n; （C1）信号耦合器1; （C2）信号耦合器n; （D1）卫星导航接收机1; （D2）卫星导航接收机
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公开(公告)号：KR101221978B1
公开(公告)日：2013-01-15
申请号：KR1020120097281
申请日：2012-09-03
Applicant: 한국항공우주연구원
Abstract: PURPOSE: A positioning tracking method of multiple jammers based on a TDOA Method is provided to accurately detect each jammer location even in case of multiple jammers. CONSTITUTION: Multiple sensors receiving GPS signals are arranged and set as reference sensors in order to calculate TDOA. (S100) The estimates of multiple jammer locations are produced based on TDOA. (S200) The multiple estimates of location are displayed on the coordinate set up based on the sensors. (S300) When search cells and search ranges are determined, by moving as a searching interval, the search cell including all true position solutions as many as the number of sensors is searched out.(S400) The number of jammers is determined and the position solutions of jammers are calculated(S500). [Reference numerals] (S100) Step of calculating a TDOA measured value; (S200) Step of calculating a position value; (S300) Step of displaying a position value; (S400) Step of setting a searching range and of searching a searching cell; (S500) Step of estimating a position
Abstract translation: 目的：提供基于TDOA方法的多个干扰器的定位跟踪方法，以便即使在多个干扰的情况下也能精确检测每个干扰位置。 规定：接收GPS信号的多个传感器被设置为参考传感器，以便计算TDOA。 （S100）基于TDOA产生多个干扰位置的估计。 （S200）位置的多个估计值基于传感器显示在设定的坐标上。 （S300）当搜索单元和搜索范围被确定时，通过作为搜索间隔移动，搜索包括与传感器的数量一样多的所有真实位置解的搜索单元（S400）确定干扰次数并且确定位置 计算干扰的解决方案（S500）。 （附图标记）（S100）计算TDOA测定值的步骤; （S200）计算位置值的步骤; （S300）显示位置值的步骤; （S400）设置搜索范围并搜索搜索单元的步骤; （S500）估计位置的步骤
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