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Patent Agency Ranking
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公开(公告)号：KR101862927B1
公开(公告)日：2018-05-30
申请号：KR1020160104208
申请日：2016-08-17
Applicant: 국방과학연구소
Abstract: 본발명은활공비행체가최적활공속도로비행하는경우의고도별최적하강률()과, 활공비행체가기준경로()를따라서비행할때 목표지점까지소요되는비행시간으로부터, 활공비행체가목표지점을통과할경우의진입고도()를예측하여, 활공비행체의진입각및 진입고도를제어하는활공비행체의진입각및 진입고도제어방법으로서, 본발명은활공비행체가적절한진입각과진입고도로목표지점을통해진입이가능하게한다.
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公开(公告)号：KR101408077B1
公开(公告)日：2014-06-18
申请号：KR1020140011713
申请日：2014-01-29
Applicant: 국방과학연구소
IPC: G05D1/10
CPC classification number: G05D1/0044 , G02B27/01 , G05D1/0038 , G05D1/101 , G06F3/013
Abstract: The present invention relates to manipulation of an unmanned aerial vehicle (UAV). A device for manipulating a UAV includes: a manipulation unit which generates a manipulation signal for manipulating the UAV; a communication unit which receives UAV data including the status data of the UAV and images acquired by the UAV from the UAV and transmits the manipulation signal to the UAV; a virtual image generation unit which creates a virtual environment for the area in which the UAV is currently located based on the current location of the UAV and generates a virtual image based on the status data of the UAV from the virtual environment; an output unit which outputs at least one among the images acquired by the UAV and the virtual image; and a control unit which inputs the current location of the UAV received from the outside and the status data of the UAV into the virtual image generation unit and controls the virtual image generation unit to generate the virtual image.
Abstract translation: 本发明涉及无人驾驶飞行器（UAV）的操纵。 一种用于操纵无人机的装置包括：操纵单元，其生成用于操纵无人机的操纵信号; 通信单元，其接收包括UAV的状态数据和UAV从UAV获取的图像的UAV数据，并将操作信号发送到UAV; 虚拟图像生成单元，其基于UAV的当前位置为UAV当前所在的区域创建虚拟环境，并且基于来自虚拟环境的UAV的状态数据生成虚拟图像; 输出单元，其输出由所述UAV获取的图像和所述虚拟图像中的至少一个; 以及控制单元，其将从外部接收的UAV的当前位置和UAV的状态数据输入到虚拟图像生成单元中，并且控制虚拟图像生成单元生成虚拟图像。
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公开(公告)号：KR1020180019909A
公开(公告)日：2018-02-27
申请号：KR1020160104208
申请日：2016-08-17
Applicant: 국방과학연구소
CPC classification number: B64D43/00 , B64D1/00 , B64D45/00 , G05D1/042 , G05D1/0676
Abstract: 본발명은활공비행체가최적활공속도로비행하는경우의고도별최적하강률()과, 활공비행체가기준경로()를따라서비행할때 목표지점까지소요되는비행시간으로부터, 활공비행체가목표지점을통과할경우의진입고도()를예측하여, 활공비행체의진입각및 진입고도를제어하는활공비행체의진입각및 진입고도제어방법으로서, 본발명은활공비행체가적절한진입각과진입고도로목표지점을통해진입이가능하게한다.
Abstract translation: 本发明基于以下发现：当滑翔飞机沿着参考路径（）行进时，从到达目标点所需的飞行时间， 本发明涉及一种控制滑翔飞机的进入角度和进入高度可控性的方法，用于通过预测进入高度来控制滑翔飞机的进入角度和进入高度 启用输入。
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