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公开(公告)号：KR1020120074472A
公开(公告)日：2012-07-06
申请号：KR1020100136316
申请日：2010-12-28
Applicant: 한국항공우주연구원
CPC classification number: G01N3/08 , G01M5/00 , G01M99/007 , G01N2203/0204 , G05B9/02
Abstract: PURPOSE: A system for controlling a stop of an aircraft structure test and a method for controlling the stop of the aircraft structure test using the same are provided to predict accumulated properties based on signals of a sensor and a fractural moment of an testing object based on a preset value while testing an aircraft structure, thereby enhancing the stability of an aircraft structure testing body and the testing object. CONSTITUTION: A system for controlling a stop of an aircraft structure test comprises a testing object(101), a testing sensor unit(103), a sensor data acquisition unit(104), a monitoring and analyzing unit(105), and a commanding unit(106). The testing object is installed in an aircraft structure testing body. The testing sensor unit is mounted on the testing object and the aircraft structure testing body. The sensor data acquisition unit receives signals from the testing sensor unit, thereby obtaining data. The monitoring and analyzing unit monitors and analyzes the obtained data. The commanding unit commands a stop of an aircraft structure test by receiving signals from the monitoring and analyzing unit.
Abstract translation: 目的：提供一种用于控制飞机结构测试停止的系统和一种用于控制飞行器结构测试停止的方法，用于基于传感器的信号和基于测试对象的断裂力矩来预测累积特性 同时测试飞行器结构的预设值，从而提高飞行器结构测试体和测试对象的稳定性。 构成：用于控制飞机结构测试停止的系统包括测试对象（101），测试传感器单元（103），传感器数据获取单元（104），监视和分析单元（105）以及命令 单元（106）。 测试对象安装在飞机结构测试机构中。 测试传感器单元安装在测试对象和飞机结构测试体上。 传感器数据采集单元从测试传感器单元接收信号，从而获得数据。 监测和分析单元监测和分析获得的数据。 指挥单位通过接收来自监测分析单元的信号来指挥飞机结构试验的停止。
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公开(公告)号：KR101091805B1
公开(公告)日：2011-12-12
申请号：KR1020090135730
申请日：2009-12-31
Applicant: 한국항공우주연구원
IPC: G08G5/00
Abstract: 본발명은자동항행감시시스템및 방법에관한것으로서, 이시스템은항공기의 3차원위치정보를생성하는 GPS 수신기, 3차원위치정보를포함하는자동항행감시메시지를방송하거나수신하는방송송수신기, 그리고 3차원위치정보를이용하여자동항행감시메시지를생성하고항공기가항법성능요구조건을충족하는지판단하는위치적합성을연산하며항공기가어느정도기준방향으로항행하고있는지판단하는방향적합성을연산하는데이터처리부를포함한다.
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公开(公告)号：KR1020110078824A
公开(公告)日：2011-07-07
申请号：KR1020090135730
申请日：2009-12-31
Applicant: 한국항공우주연구원
IPC: G08G5/00
CPC classification number: G08G5/0013 , G08G5/0017 , G08G5/003
Abstract: PURPOSE: An automatic dependent surveillance-broadcast system and an automatic dependent surveillance-broadcast method are provided to grasp the direction and location of an airplane by using three dimensional location information. CONSTITUTION: A GPS receiver(140) generates the three dimensional location information of an airplane. A broadcast transceiver(120) broadcasts and receives an automatic dependent surveillance message including the three dimensional location information. A data processor(110) generates the automatic dependent surveillance message including the three dimensional location information and operates direction suitability.
Abstract translation: 目的：提供自动相关监控广播系统和自动依赖监控广播方法，通过使用三维位置信息来掌握飞机的方向和位置。 构成：GPS接收器（140）产生飞机的三维位置信息。 广播收发机（120）广播并接收包括三维位置信息的自动依赖监视消息。 数据处理器（110）产生包括三维位置信息的自动依赖监视消息并且操作方向适应性。
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Patent Agency Ranking
公开(公告)号：KR1020100071428A
公开(公告)日：2010-06-29
申请号：KR1020080130136
申请日：2008-12-19
Applicant: 한국항공우주연구원
CPC classification number: H04L41/145 , H04L1/203 , H04W24/06
Abstract: PURPOSE: A communication environment simulation server and a communication environment simulating method thereof are provided to determine the class of a communication environment in response to the current position information of a moving object. CONSTITUTION: If a test signal is received from a moving object, a position tracing unit(120) tracks the current position of the moving object. An information reading unit reads the received signal bit information corresponding to the current position information of the moving body from a movement information table. A BER(Bit Error Rate) production unit(160) produces a BER by comparing the received signal bit information with the bit information of the test signal. A communication environment determining unit(170) determines the communications environment corresponding to the current position information of the moving object through the BER.
Abstract translation: 目的：提供通信环境模拟服务器及其通信环境模拟方法，以响应于移动对象的当前位置信息来确定通信环境的类别。 构成：如果从移动物体接收到测试信号，则位置跟踪单元（120）跟踪移动物体的当前位置。 信息读取单元从移动信息表读取与移动体的当前位置信息对应的接收信号位信息。 BER（误码率）产生单元（160）通过将接收到的信号位信息与测试信号的比特信息进行比较来产生BER。 通信环境确定单元（170）通过BER确定与移动物体的当前位置信息相对应的通信环境。
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公开(公告)号：KR100980762B1
公开(公告)日：2010-09-10
申请号：KR1020070137052
申请日：2007-12-26
Applicant: 한국항공우주연구원
Inventor： 송재훈
IPC: G01S5/14
Abstract: 본 발명은 GPS 신호를 이용하여 항공기의 정밀 접근 및 착륙을 위한 지상기반 위성항법 보강시스템(Ground Based Augmentation System, 이하 GBAS)을 위한 통신제어장치에 관한 것이다.
이를 위한 본 발명은 지상시스템 및 항공기 탑재시스템으로 구성되며 GPS 신호를 이용하여 항공기의 정밀 접근 및 착륙을 위한 지상기반 위성항법 보강시스템(GBAS)에 있어서, 상기 GPS 신호를 수신하는 지상 GPS 안테나(10) 및 탑재 GPS 안테나(10')의 3차원 위치 계산을 위한 항법 데이터를 제공하는 지상시스템용 GPS 수신기(20) 및 탑재시스템용 GPS 수신기(20')로부터 상기 항법 데이터를 이용하여 상기 지상 GPS 안테나(10) 및 탑재 GPS 안테나(10')의 현재 위치를 실시간으로 계산하는 지상시스템용 신호처리장치(30) 및 탑재시스템용 신호처리장치(30')와 상기 지상시스템용 신호처리장치(30) 및 탑재시스템용 신호처리장치(30')를 통하여 계산되는 데이터를 송수신하는 VDB 송신 무선모뎀(50) 및 VDB 수신 무선모뎀(50')사이에 구비되어 GBAS 메시지 형식 자동 생성 및 해석을 수행하는 것을 특징이 있다.
GBAS, 통신제어장치, 신호처리장치, VDB 무선 모뎀-
公开(公告)号：KR1020090069403A
公开(公告)日：2009-07-01
申请号：KR1020070137052
申请日：2007-12-26
Applicant: 한국항공우주연구원
Inventor： 송재훈
IPC: G01S5/14
Abstract: A communication controller unit for ground based augmentation system is to provide the production of GBAS(ground based augmentation system) message of standard and interpretative function by forming interface between VDB(VHF data broadcast) transmitting and receiving wireless MODEM. The ground GPS antenna(10) receives the GPS signal. The GPS receiver(20) for the ground system provides navigational data for 3D position calculation. The signal processing unit(30) for the ground system calculates the current position of the ground GPS antenna in real time by using navigational data. The VDB transmit radio modem(50) transmits calculated data through the signal processing unit.
Abstract translation: 用于地面增强系统的通信控制器单元通过形成VDB（VHF数据广播）发送和接收无线MODEM之间的接口来提供标准和解释功能的GBAS（地面增强系统）消息的生成。 地面GPS天线（10）接收GPS信号。 用于地面系统的GPS接收机（20）提供用于3D位置计算的导航数据。 用于地面系统的信号处理单元（30）通过使用导航数据实时地计算地面GPS天线的当前位置。 VDB发射无线电调制解调器（50）通过信号处理单元发送计算的数据。
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公开(公告)号：KR1020090069412A
公开(公告)日：2009-07-01
申请号：KR1020070137065
申请日：2007-12-26
Applicant: 한국항공우주연구원
Inventor： 송재훈
IPC: G01S5/14
Abstract: A cockpit display of traffic information for automatic dependent surveillance-broadcast is provided to secure the safety by providing the emergency signal and attention function about the abnormal situation. The antenna(10) is installed outside an aircraft and a moving body. The ADS-B transmitter(20) broadcasts the ADS-B message including the location information of the moving body to the aircraft, and the moving body and the ground system. The ADS-B receiver(30) receives each ADS-B message broadcasted by the aircraft, and the moving body and ground system through the antenna. The GPS receiver(60) provides three dimensional position of the GPS antenna(50) as 3D coordinate. The data processing unit(40) recieves 3D coordinate from the GPS receiver and produces the ADS-B message. The ADS-B message received in the ADS-B receiver is translated.
Abstract translation: 提供用于自动相关监控广播的交通信息的驾驶舱显示，以通过提供关于异常情况的紧急信号和关注功能来确保安全。 天线（10）安装在飞机外部和移动体上。 ADS-B发射机（20）将包括移动体的位置信息的ADS-B消息广播到飞行器，以及移动体和地面系统。 ADS-B接收机（30）通过天线接收飞机广播的每个ADS-B消息，以及移动体和地面系统。 GPS接收器（60）将GPS天线（50）的三维位置提供为3D坐标。 数据处理单元（40）从GPS接收器接收3D坐标并产生ADS-B消息。 在ADS-B接收机中接收的ADS-B消息被翻译。
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公开(公告)号：KR1020140091963A
公开(公告)日：2014-07-23
申请号：KR1020130004047
申请日：2013-01-14
Applicant: 한국항공우주연구원 , 한국과학기술원 , 단암시스템즈 주식회사
CPC classification number: B64D45/00 , B64C3/185 , B64C3/187 , B64C2009/005 , B64D2045/0085 , B64F5/60
Abstract: The present invention provides a real-time safety inspection system (1000) for an ultralight aircraft to monitor the safety of an ultralight aircraft (1) in real time, wherein the ultralight aircraft includes a fuselage (10) having a cockpit (11); and main wings (20), each of which has a spar (21), a rib (22), a plank (23) wrapped around the spar (21) and the rib (22), and an aileron (24) hinged and coupled at the plank (23), to be combined on both sides of the fuselage (10). The real-time safety inspection system includes an optical sensor (100) buried in the main wing (20) for measuring the weight and the temperature; a piezoelectric sensor (200) buried in the main wing (20) for measuring vibration; an acceleration sensor (300) buried in the aileron (24) for measuring a shock amount; and a central control part (400) installed in the cockpit (11) for processing and displaying measured data of all the sensors.
Abstract translation: 本发明提供一种用于超轻型飞机实时监控超轻型飞机（1）的安全性的实时安全检查系统（1000），其中超轻型飞机包括具有座舱（11）的机身（10）; 和主翼（20），每个主翼具有翼梁（21），肋（22），围绕翼梁（21）和肋（22）缠绕的板条（23）以及铰链和 耦合在板条（23）上，以组合在机身（10）的两侧。 实时安全检查系统包括：掩埋在主翼（20）中的光学传感器（100），用于测量重量和温度; 埋置在所述主翼（20）中用于测量振动的压电传感器（200）; 掩埋在所述副翼（24）中的用于测量冲击量的加速度传感器（300） 以及安装在驾驶舱（11）中的中央控制部（400），用于处理和显示所有传感器的测量数据。
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