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

公开(公告)号：KR1020130022635A

公开(公告)日：2013-03-07

申请号：KR1020110085360

申请日：2011-08-25

Applicant: 한국항공우주연구원

Inventor： 김해동

IPC: B64G1/10 ,  B64G3/00 ,  H04B7/185

CPC classification number: B64G1/10 ,  B64G1/242 ,  B64G3/00 ,  G05D1/0883 ,  H04B7/185

Abstract: PURPOSE: A NORAD TLE(North American Aerospace Defense Command Two-line Elements) data-based orbit determination system and a method thereof are provided to obtain high precision of position information by utilizing NORAD TLE data receiving from a JSPOC(Joint Space Operations Center) as pseudo measurement data. CONSTITUTION: A NORAD TLE data-based orbit determination system comprises a TLE preprocessing part(100), an orbit determining part(200), and a position information output part(300). The TLE preprocessing part propagates NORAD data to an SGP-based orbit propagator to obtain position data on an ECI(Earth-Centered Inertial) coordinate system; converts the position data on the ECI coordinate system to position data on an ECEF(Earth-Centered-Earth-Fixed) coordinate system; and converts the converted position data on the EDEF coordinate system to PCE format position data. The orbit determining part determines information on the position of an orbit determining target through a batch processing technique by using the PCE format position data as pseudo measurement data. The position information output part converts the information on the position of the orbit determining target to a preset data format and outputs the data. [Reference numerals] (100) TLE preprocessing part; (200) Orbit determining part; (300) Position information output part

Abstract translation: 目的：提供一种基于数据的轨道确定系统的NORAD TLE（北美航空航天防务指挥系统）的轨道确定系统及其方法，以通过利用从JSPOC（联合太空作战中心）接收的NORAD TLE数据来获得位置信息的高精度， 作为伪测量数据。 构成：NORAD TLE基于数据的轨道确定系统包括TLE预处理部分（100），轨道确定部分（200）和位置信息输出部分（300）。 TLE预处理部分将NORAD数据传播到基于SGP的轨道传播器，以获取ECI（以地心为中心的）惯性坐标系的位置数据; 将ECI坐标系上的位置数据转换为在ECEF（以地球为中心的地球固定）坐标系上的位置数据; 并将EDEF坐标系上的转换位置数据转换为PCE格式位置数据。 轨道确定部通过使用PCE格式位置数据作为伪测量数据，通过批量处理技术来确定关于轨道确定目标的位置的信息。 位置信息输出部将关于轨道确定对象的位置的信息转换为预设的数据格式，并输出该数据。 （附图标记）（100）TLE预处理部; （200）轨道确定部分; （300）位置信息输出部

公开(公告)号：KR101082325B1

公开(公告)日：2011-11-10

申请号：KR1020090135242

申请日：2009-12-31

Applicant: 한국항공우주연구원

Inventor： 김해동

IPC: G06F17/21 ,  G06F19/00

Abstract: 본발명은위성별각 항목의스크립트정의및 각항목사이의상관관계를스크립트언어를이용하여입력하는스크립트입력부, 상기스크립트입력부를통해입력된위성별각 항목의정의를저장하는항목데이터베이스, 상기스크립트입력부를통해입력된각 항목사이의상관관계를저장하는항목관계데이터베이스, 각위성별요청서파일형식, 항목의기재위치정보를포함하는요청서포맷정보가스크립트언어로정의되어저장되는요청서포맷데이터베이스, 외부로부터접수되는요청서를상기요청서포맷데이터베이스에저장된요청서포맷정보를이용하여 XML 파일형식으로변환시키는인터프리터부, 상기인터프리터부에의해변환된요청서를이용하여임무계획표를생성하는스케줄러를포함하는범용임무계획시스템을제공한다.

公开(公告)号：KR100651617B1

公开(公告)日：2006-12-01

申请号：KR1020050123556

申请日：2005-12-15

Applicant: 한국항공우주연구원

Inventor： 김도형 ,  김해동 ,  김승호

IPC: B64C27/32

Abstract: A hingeless rotor apparatus having stacked type flexures is provided to reduce a manufacturing cost by acquiring stability through a coupling stiffness without an additional apparatus such as a lead-lad damper. A hingeless rotor apparatus having stacked type flexures includes a rotor shaft connection unit(110), a plurality of blades(300), and a plurality of flexures. The plurality of blades are rotated by the rotor shaft connection unit. An end of the plurality of flexures is connected to a hub, and the other end of the plurality of flexures is connected to the blade. The flexures are stacked by a plurality of free flag layers having reinforced fiber and material. Any one of the plurality of composite material layers has a differently arranged reinforced fiber from a reinforced fiber length direction of the different layer.

Abstract translation: 提供具有堆叠型挠曲件的无铰链转子装置，以通过在没有额外装置如铅 - 铅阻尼器的情况下通过耦合刚度获得稳定性来降低制造成本。 具有堆叠型挠曲件的无铰链转子装置包括转子轴连接单元（110），多个叶片（300）以及多个挠曲件。 多个叶片由转子轴连接单元旋转。 多个挠曲件的一端连接至轮毂，并且多个挠曲件的另一端连接至叶片。 挠曲件由多个具有增强纤维和材料的自由旗帜层堆叠。 多个复合材料层中的任何一个具有与不同层的增强纤维长度方向不同排列的增强纤维。