公开(公告)号：KR101491924B1

公开(公告)日：2015-02-11

申请号：KR1020130100259

申请日：2013-08-23

Applicant: 한국항공우주연구원

Inventor： 이상철 ,  류동영 ,  김정훈 ,  김해동 ,  김인규 ,  문상만 ,  한상혁 ,  문성태 ,  김진원 ,  조동현 ,  공현철 ,  김민기 ,  김종철

IPC: E04H6/00 ,  E04H6/12

CPC classification number: E04H6/44 ,  B64F1/04 ,  E01F3/00

Abstract: 이착륙 비행체의 타워형 충전 및 격납시스템이 개시된다. 복수개의 비행체를 격납시키며 충전시킬 수 있는 타워에 있어서, 타워 외벽에서 펼쳐져 나옴으로써, 비행체가 착륙하며, 복수개로 구성된 착륙부, 착륙부에서 비행체를 자동착륙 시킬 수 있는 자동착륙부, 비행체를 격납하며 충전하며, 상태 데이터 모니터링을 하는 격납장치부, 비행체가 이상이 있을 경우 수리할 수 있는 유지보수실, 타워내부에 구비된 엘레베이터, 엘레베이터로 인하여 수직 혹은 수평이동을 하여 착륙부에 있는 비행체를 결합시켜 격납장치부 혹은 유지보수실에 장착시키는 로봇암으로 구성된다. 복수개의 무인기를 이착륙 및 격납 충전 할 수 있어 관리하기 쉬워 운용의 효율성을 증가시키며, 수직으로 무인기를 복수개 배치시킴으로써 공간활용을 높일수 있다.

Abstract translation: 公开了一种塔式系统，用于起飞和着陆飞行器的充电和收容。 塔架系统包括：从塔的外壁拉伸到陆上飞行器的多个着陆单元; 自动着陆单元，允许着陆单元自动着陆飞行器; 住房设备单元，用于容纳和充电飞行车辆并监视状态数据; 修理异常飞行车辆的维修室; 安装在塔架中的电梯; 以及通过电梯垂直或水平移动的机器人臂，以将层站单元中的飞行车辆联接以安装在壳体装置单元或维护室中。 根据本发明，多个无人驾驶飞行器可以起飞，着陆，收纳和充电，从而通过易于管理提高操作效率，并通过垂直安装无人驾驶飞行器来提高空间可用性。

公开(公告)号：KR101413919B1

公开(公告)日：2014-07-01

申请号：KR1020130050625

申请日：2013-05-06

Applicant: 한국항공우주연구원

Inventor： 조동현 ,  김종철

IPC: G06F17/10

CPC classification number: G06N7/023

Abstract: Provided is a device for controlling a kite by using a fuzzy controller. The device for controlling the kite comprises a modeling unit and a control unit. The modeling unit performs mathematical modeling by using a motion equation related to the kite. The control unit controls the modeled kite by using at least one variable of state of the fuzzy controller.

Abstract translation: 提供了一种通过使用模糊控制器控制风筝的装置。 用于控制风筝的装置包括建模单元和控制单元。 建模单元通过使用与风筝相关的运动方程来执行数学建模。 控制单元通过使用模糊控制器的状态的至少一个变量来控制建模的风筝。

公开(公告)号：KR1020100048614A

公开(公告)日：2010-05-11

申请号：KR1020080107862

申请日：2008-10-31

Applicant: 한국항공우주연구원

Inventor： 김종철

IPC: B63H9/04 ,  B63H9/06

CPC classification number: B63H9/06 ,  C25B1/04 ,  Y02E10/725

Abstract: PURPOSE: A hydrocarbon fuel production vessel using wind power generation and electrolysis is provided to produce a hydrocarbon fuel by electrolyzing sea water with electricity generated by a propeller and using the generated hydrogen and carbon dioxide in the air. CONSTITUTION: A hydrocarbon fuel production vessel using wind power generation and electrolysis comprises a paraglider(10) fixed with a first wire(11) to a vessel(1) and propelling the vessel with the lifting force perpendicular to the wind direction, a first winding device(20) which rolls or unrolls the first wire connected to the paraglider, a generator(40) driven with a propeller(30) rotated when propelling the vessel, a reactor(50) electrolyzing sea water the electricity created from the generator, and a carbon dioxide collector(60) collecting the carbon dioxide in the atmosphere and supplies to the reactor.

Abstract translation: 目的：提供使用风力发电和电解的碳氢化合物燃料生产容器，通过用螺旋桨产生的电力并利用空气中产生的氢和二氧化碳电解海水来生产碳氢化合物燃料。 构成：使用风力发电和电解的碳氢化合物燃料生产容器包括用第一线（11）固定到容器（1）并以垂直于风向推进的推进船的滑翔伞（10），第一绕组 装置（20），其滚动或展开连接到滑翔机的第一线;由推进船舶时旋转的螺旋桨（30）驱动的发电机（40）;电解海水从发电机产生的电力的电抗器（50）;以及 二氧化碳收集器（60），其收集大气中的二氧化碳并将其供应到反应器。

公开(公告)号：KR100380112B1

公开(公告)日：2003-04-11

申请号：KR1020000083439

申请日：2000-12-28

Applicant: 한국항공우주연구원

Inventor： 김종철

IPC: G01S5/02

Abstract: PURPOSE: A time synchronization signal insertion transmitter/receiver of a global positioning system compensating signal is provided to load additional time information through an ASK modulation using an orthogonality of a signal without damaging DGPS information according to an MSK modulation. CONSTITUTION: An antenna(1) receives a GPS signal. An MSK modulator(6) loads calculated global positioning system compensating information in an intermediate wave. An ASK modulator(8) loads time information received and divided by the antenna(1) in an MSK modulating signal from the MSK modulator(6). A transmitter(10) transmits a final modulating signal modulated by the MSK modulator(6). A demodulator converts a signal received through a receiving antenna into a base band signal. A carrier wave mixer generates a carrier wave signal. An A/D converter converts an analog signal from a module into a digital signal. A DSP module demodulates the digital signal from the A/D converter in parallel and obtains global positioning system information and time information. An interface controller controls a total system.

Abstract translation: 目的：提供全球定位系统补偿信号的时间同步信号插入发射机/接收机，以根据MSK调制通过使用信号的正交性的ASK调制来加载附加时间信息，而不损坏DGPS信息。 构成：天线（1）接收GPS信号。 MSK调制器（6）将计算出的全球定位系统补偿信息加载到中间波中。 ASK调制器（8）将来自MSK调制器（6）的MSK调制信号加载由天线（1）接收并划分的时间信息。 发射机（10）发射由MSK调制器（6）调制的最终调制信号。 解调器将通过接收天线接收的信号转换为基带信号。 载波混频器产生载波信号。 A / D转换器将来自模块的模拟信号转换为数字信号。 DSP模块并行解调来自A / D转换器的数字信号，并获得全球定位系统信息和时间信息。 接口控制器控制整个系统。

公开(公告)号：KR1020030006218A

公开(公告)日：2003-01-23

申请号：KR1020010041911

申请日：2001-07-12

Applicant: 한국항공우주연구원

Inventor： 김종철 ,  오경륜

IPC: G01S5/14

Abstract: PURPOSE: A time synchronization signal insertion satellite navigation compensation signal transmitting/receiving system is provided to exactly confirm a time slot interval of a received signal in a receiver side by inserting a data synchronization signal into time information while maintaining an RTCM format. CONSTITUTION: A transmitting system includes a satellite navigation receiver(2), an atomic timepiece(6), and a data link part(12). The satellite navigation receiver receives a GPS signal and generates difference compensation message. The atomic timepiece(6) in a reference center generates time information in which 1 pps synchronous signal is inserted. The data link part(12) modulates and transmits the difference compensation message and time information to a user. A receiving system includes a data link part and a satellite navigation receiver. The data link part demodulates and obtains the difference compensation message and time information. The satellite navigation receiver displays and outputs a final navigation information location coordinate.

Abstract translation: 目的：提供时间同步信号插入式卫星导航补偿信号发送/接收系统，通过在保持RTCM格式的同时将数据同步信号插入到时间信息中来准确地确认接收机侧的接收信号的时隙间隔。 构成：发射系统包括卫星导航接收器（2），原子钟表（6）和数据链接部分（12）。 卫星导航接收机接收GPS信号并产生差分补偿消息。 参考中心中的原子钟表（6）产生插入1pps同步信号的时间信息。 数据链接部分（12）将差分补偿消息和时间信息调制并发送给用户。 接收系统包括数据链路部分和卫星导航接收机。 数据链路部分解调并获得差分补偿消息和时间信息。 卫星导航接收机显示并输出最终的导航信息位置坐标。