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公开(公告)号：KR101695899B1
公开(公告)日：2017-01-23
申请号：KR1020160000978
申请日：2016-01-05
Applicant: 한국항공우주연구원
CPC classification number: B63B17/00 , B63B35/00 , B64C39/02 , B64D47/00 , B64D47/08 , G06K9/20 , G06Q50/10
Abstract: 비행체를이용한해양감시시스템이개시되어있다.개시된비행체를이용한해양감시시스템은유인또는무인선박에장착되어, 주변의특정선박의선박자동식별유닛에서발신되는선박식별정보를수신하는수신유닛; 상기유인또는무인선박에장착된촬영유닛에의해촬영된영상정보를전기신호로변환하되, 주간영상센서나적외선센서, SAR(Synthetic Aperture Radar, 합성개구레이더), LiDAR 등의전파를이용한시현장치중 어느하나로되는영상센서; 상기수신유닛과영상센서로부터수신되는두 정보를융합하여디스플레이부에특정선박의영상과그 선박의식별정보를중첩해서출력되도록제어하는제어부;로이루어지되, 상기제어부는상기유인또는무인선박에설치됨을더 포함하며, 상기디스플레이부에출력되는영상은실시간으로선박영상의화질을개선하여안개를제거하거나, 영상의흔들림을보정하는보정유닛이구비됨을더 포함하고, 상기디스플레이부에는상기영상센서의근접영역내에위치한단일또는다수의선박이출력됨을더 포함하며, 상기선박식별유닛으로부터받은선박의위치와선박의진행방향이도시되는전자지도를더 포함하되, 전자지도상에서해당선박을마우스나화면터치방식으로선택하는경우선박식별유닛으로부터확득한선박이름을포함하는하나이상의정보가출력되며, 이와함께, 비행체의위치와진행방향이도시되고, 비행체의영상센서가지향하는목표점도도시되는것을특징으로한다.
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Patent Agency Ranking
公开(公告)号：KR1020150027554A
公开(公告)日：2015-03-12
申请号：KR1020130106103
申请日：2013-09-04
Applicant: 한국항공우주연구원
Abstract: 노브 다이얼을 이용한 엔진 추력 입력장치 및 입력방법이 개시된다. 화면 전환단계, 엔진시동 선택창의 락 버튼 생성단계, 락 버튼을 해제한 후, START 버튼을 눌러 엔진의 시동을 켤 수 있는 엔진추력 활성화 단계, 지상 공회전(GI)입력단계, 비행 공회전(FI)입력단계, 화면전환단계를 포함하여 구성된다. 지상 공회전(GI)입력단계 혹은 비행 공회전(FI)입력단계는 지상 공회전의 노브값 100 근방, 비행 공회전의 노브값 200근방으로 숫자를 올림으로써 엔진 추력을 발생시켜, 비행공회전 이하로 스틱을 조절하지 않아도 되며, 조종사가 실수로 잘못된 값을 설정할 가능성이 줄어 추력이 갑자기 내려가는 위험적인 요인을 줄일 수 있으며, 입력이 간편하여 업무의 효율성을 향상시킬 수 있다.
Abstract translation: 在本发明中公开了使用旋钮拨盘的发动机推力输入装置及其输入方法。 输入方法包括：屏幕切换步骤; 发动机点火选择窗口上的锁定按钮生成步骤; 发动机推力启动步骤，其可以通过按下START按钮来点燃发动机; 地面空闲（GI）输入步骤; 战斗空闲（FI）输入步骤; 和屏幕切换步骤。 GI输入步骤或FI输入步骤可以通过将数字增加到GI的大约旋钮值100，并且对于FI围绕旋钮值200，来产生发动机推力。 因此，输入方式可以消除FI下调节棒的需要，通过减少驾驶员错误设定错误值的可能性，减少突然推力下降的危险因素，通过方便的输入可以提高工作效率。
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公开(公告)号：KR1020140084615A
公开(公告)日：2014-07-07
申请号：KR1020120154260
申请日：2012-12-27
Applicant: 한국항공우주연구원
IPC: G06T17/05
CPC classification number: G06T17/05 , G01C11/02 , G06T7/40 , G06T2207/10032
Abstract: Disclosed is a device to process an image. The device to process an image comprises: a database to store 3D model data including geometric information and texture information about the topography of a target area related to the flight of an aircraft; and a rendering unit to render a first image of the topography seen from a first viewpoint corresponding to the viewpoint of a mission camera of the aircraft.
Abstract translation: 公开了一种处理图像的装置。 用于处理图像的设备包括：数据库，用于存储3D模型数据，包括关于与飞行器的飞行有关的目标区域的地形的几何信息和纹理信息; 以及渲染单元，用于呈现从对应于飞行器的任务摄像机的视点的第一视点看到的地形的第一图像。
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公开(公告)号：KR1020090082008A
公开(公告)日：2009-07-29
申请号：KR1020080008229
申请日：2008-01-25
Applicant: 한국항공우주연구원
Abstract: An actuator drive control device of a dual structure in an unmanned aerial vehicle and the method are provided to improve fault tolerance for heightening the reliability of an unmanned aerial vehicle. An actuator drive control device(103) of a dual structure in an unmanned aerial vehicle comprises communication modules communicating with a flight control computer, a first DSP(113) controlling an actuator according to the order of the flight control computer, a first MSP(105) diagnosing whether the first DSP operates normally or not, and whether a first channel malfunctions or not, a second DSP(121) controlling an actuator subordinately to the first DSP or independently, and a second MSP(117) diagnosing whether the second DSP operates normally or not, and whether the first channel malfunctions or not, and exchanging the data with the first MSP.
Abstract translation: 提供了一种无人驾驶飞行器双重结构的致动器驱动控制装置，并且提供了用于提高容错度以提高无人驾驶飞行器的可靠性的方法。 无人飞行器中的双重结构的致动器驱动控制装置（103）包括与飞行控制计算机通信的通信模块，根据飞行控制计算机的顺序控制致动器的第一DSP（113），第一MSP（ 105）诊断第一DSP是否正常运行以及第一通道是否发生故障，第二DSP（121）是否依次控制第一DSP或独立地执行致动器;以及第二MSP（117），其诊断第二DSP 是否正常工作，以及第一个通道是否发生故障，以及与第一个MSP交换数据。
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公开(公告)号：KR100856688B1
公开(公告)日：2008-09-04
申请号：KR1020070035547
申请日：2007-04-11
Applicant: 한국항공우주연구원
IPC: B64C27/28
Abstract: An envelope protection controller and a tiltrotor aircraft having the same are provided to protect an envelope by automatically adding and subtracting a nacelle tilting order when deviating from the envelope. An envelope protection controller includes an input module, a first control module, a second control module, and a manual nacelle switch(61). The input module receives a target speed, an acceleration order, or a tilting order. The first control module receives a nacelle tilting order for changing a nacelle angle according to the input by the input module. The second control module maintains the nacelle angle within the envelope by automatically receiving a new nacelle tilting order by a conversion order(52) with respect to a predetermined speed reference value when the nacelle angle changed according to the nacelle tilting order deviates from a previously stored transition envelope. The manual nacelle switch releases the envelope protection controller to manually convert it.
Abstract translation: 提供一种信封保护控制器和具有该信封的倾转旋翼飞机，以在偏离信封时自动增加和减去机舱倾斜命令来保护信封。 信封保护控制器包括输入模块，第一控制模块，第二控制模块和手动机舱开关（61）。 输入模块接收目标速度，加速顺序或倾斜顺序。 第一控制模块根据输入模块的输入接收用于改变机舱角度的机舱倾斜顺序。 当机舱角度根据机舱倾斜顺序改变偏离先前存储的机舱倾斜顺序时，第二控制模块通过相对于预定速度参考值通过转换顺序（52）自动接收新的机舱倾斜顺序来将机舱角度保持在包络内 过渡包络 手动机舱开关释放信封保护控制器进行手动转换。
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公开(公告)号：KR1020040004955A
公开(公告)日：2004-01-16
申请号：KR1020020039198
申请日：2002-07-08
Applicant: 한국항공우주연구원
IPC: B64D43/00
Abstract: PURPOSE: A pressure sensor is used to measure pressure difference between both wings of an airplane, thereby measuring position angle of the wings. CONSTITUTION: More than two pressure measuring members(10) are installed in both wings of an airplane through atmosphere connection pipes(2,3). A loaded computer(4) is installed to calculate position angle with the measured pressure of the pressure measuring members.
Abstract translation: 目的：使用压力传感器来测量飞机两翼之间的压力差，从而测量机翼的位置角度。 构成：通过大气连接管（2,3），两个以上的压力测量部件（10）安装在飞机的两翼上。 装载的计算机（4）被安装以用测量的压力测量构件的压力来计算位置角度。
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