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    수직무인이착륙 비행체의 충전 및 격납을 위한 운송체 및 그 방법
    4.
    发明公开
    수직무인이착륙 비행체의 충전 및 격납을 위한 운송체 및 그 방법 有权
    用于不定期垂直起降飞机的充电和包含车辆及其方法

    公开(公告)号：KR1020130122715A

    公开(公告)日：2013-11-08

    申请号：KR1020130125151

    申请日：2013-10-21

    Applicant: 한국항공우주연구원

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

    IPC: B64F1/12 ,  B64F3/02 ,  B64F1/18

    Abstract: Disclosed are a vehicle for charging and containing vertical unmanned take-off and landing aircraft and a method thereof. A moving type charging and containing transport vehicle capable of containing and charging a plurality of aircrafts comprises a movable container accommodating the aircrafts, a landing part opening or closing outer sides of the container, a landing place making a plurality of aircraft lands, a data monitoring part monitoring state data by containing and charging the aircraft, and a communication switching part communicating with the aircraft. A container vehicle, if existing only at a fixed place, has a limited operation range because of a limit of a battery of an unmanned aircraft, but if movable, can operate, charge and contain the unmanned aircraft even at the place where the unmanned aircraft can go. The container vehicle can reduce movement time of the aircraft and increase operation efficiency.

    Abstract translation: 公开了一种用于充电和容纳垂直无人飞机和着陆飞机的车辆及其方法。 一种能够容纳和充电多台飞机的移动式充电和运输车辆包括容纳飞行器的可移动容器，容器的打开或关闭外侧的着陆部分，制造多个飞机地面的着陆部位，数据监视 通过包含和充电飞机的部分监视状态数据，以及与飞行器通信的通信切换部分。 一个集装箱车辆，如果仅在固定的地方存在，由于无人驾驶飞机的电池的限制，操作范围有限，但如果是可移动的，则可以在无人驾驶飞机的地方进行操作，收取和控制无人飞机 可以去。 集装箱车辆可以减少飞机的运动时间并提高运行效率。

    위성 시뮬레이터를 위한 초기데이터 추출 및 예측 시스템
    5.
    发明授权
    위성 시뮬레이터를 위한 초기데이터 추출 및 예측 시스템 有权
    卫星仿真器的初始状态提取和估计系统

    公开(公告)号：KR101278554B1

    公开(公告)日：2013-06-25

    申请号：KR1020110147376

    申请日：2011-12-30

    Applicant: 한국항공우주연구원

    Inventor： 이상철 ,  김해동 ,  임정흠 ,  석진영

    IPC: G06F19/00

    CPC classification number: G06F17/5009 ,  G06N5/04

    Abstract: PURPOSE: A system for extracting and predicting initial data for a satellite simulator is provided to estimate the state of a satellite in the ground when an abnormality of the satellite is generated and generate a proper restoration procedure, thereby restoring the satellite. CONSTITUTION: A receiving unit(310) receives initial satellite state data and initial flight dynamic data. A data extracting device(320) extracts satellite state data and flight dynamic data from the initial satellite state data and the initial flight dynamic data. A data estimating device(330) predicts satellite state data and flight dynamic data of a future time point from the satellite state data and the flight dynamic data. The data estimating device includes a filter(335) and a dynamic model unit(336) connected to the filter. The initial satellite state data is received from a real-time operating system of a ground control system. [Reference numerals] (215) Initial flight dynamic data; (235) Initial satellite state data; (336) Dynamic model; (400) Satellite simulator

    Abstract translation: 目的：提供卫星模拟器的初始数据提取和预测系统，以便在卫星异常产生时估计卫星的状态，并产生适当的恢复过程，从而恢复卫星。 构成：接收单元（310）接收初始卫星状态数据和初始飞行动态数据。 数据提取装置（320）从初始卫星状态数据和初始飞行动态数据中提取卫星状态数据和飞行动态数据。 数据估计装置（330）从卫星状态数据和飞行动态数据预测未来时间点的卫星状态数据和飞行动态数据。 数据估计装置包括连接到滤波器的滤波器（335）和动态模型单元（336）。 从地面控制系统的实时操作系统接收初始卫星状态数据。 （附图标记）（215）初始飞行动态数据; （235）初始卫星状态数据; （336）动态模型; （400）卫星模拟器

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