公开(公告)号：US07840351B2

公开(公告)日：2010-11-23

申请号：US11718234

申请日：2005-11-04

申请人： Yoo-La Hwang ,  Byoung-Sun Lee ,  Jae-Hoon Kim

发明人： Yoo-La Hwang ,  Byoung-Sun Lee ,  Jae-Hoon Kim

IPC分类号： G01C21/00

CPC分类号： G01S19/07

摘要： Provided is a method of correcting an ionosphere error, a system of a precise orbit determination using the same and a method thereof. The method includes the steps of: a) determining a time of a highest elevation angle of a GPS satellite per one pass of each GPS satellite received at a LEO satellite or a receiver on a ground; b) determining a minimum total electron content found from an ionosphere model of the determined time per one pass of each GPS satellite; c) determining a total electron content directly calculated from the LEO satellite or a single frequency GPS data; d) determining an ionosphere error value of a single frequency GPS data by combining the minimum total electron content and the directly calculated total electron content; and e) correcting pseudorange data or carrier phase data based on the determined ionosphere error value.

摘要翻译： 提供了一种校正电离层误差的方法，使用其的精确轨道确定系统及其方法。 该方法包括以下步骤：a）确定在LEO卫星或地面接收机处接收的每个GPS卫星的每次通过GPS卫星的最高仰角的时间; b）确定从每个GPS卫星的每次通过确定的时间的电离层模型中发现的最小总电子含量; c）确定从LEO卫星直接计算的总电子量或单频GPS数据; d）通过组合最小总电子含量和直接计算的总电子含量来确定单频GPS数据的电离层误差值; 以及e）基于确定的电离层误差值来校正伪距数据或载波相位数据。

公开(公告)号：US20090091493A1

公开(公告)日：2009-04-09

申请号：US11718234

申请日：2005-11-04

申请人： Yoo-La Hwang ,  Byoung-Sun Lee ,  Jae-Hoon Kim

发明人： Yoo-La Hwang ,  Byoung-Sun Lee ,  Jae-Hoon Kim

IPC分类号： G01S5/14

CPC分类号： G01S19/07

摘要： Provided is a method of correcting an ionosphere error, a system of a precise orbit determination using the same and a method thereof. The method includes the steps of: a) determining a time of a highest elevation angle of a GPS satellite per one pass of each GPS satellite received at a LEO satellite or a receiver on a ground; b) determining a minimum total electron content found from an ionosphere model of the determined time per one pass of each GPS satellite; c) determining a total electron content directly calculated from the LEO satellite or a single frequency GPS data; d) determining an ionosphere error value of a single frequency GPS data by combining the minimum total electron content and the directly calculated total electron content; and e) correcting pseudorange data or carrier phase data based on the determined ionosphere error value.

摘要翻译： 提供了一种校正电离层误差的方法，使用其的精确轨道确定系统及其方法。 该方法包括以下步骤：a）确定在LEO卫星或地面接收机处接收的每个GPS卫星的每次通过GPS卫星的最高仰角的时间; b）确定从每个GPS卫星的每次通过确定的时间的电离层模型中发现的最小总电子含量; c）确定从LEO卫星直接计算的总电子量或单频GPS数据; d）通过组合最小总电子含量和直接计算的总电子含量来确定单频GPS数据的电离层误差值; 以及e）基于确定的电离层误差值来校正伪距数据或载波相位数据。

公开(公告)号：US20060136103A1

公开(公告)日：2006-06-22

申请号：US10536601

申请日：2003-09-26

申请人： Byoung-Sun Lee ,  Jeong-Sook Lee ,  Hee-Sook Mo ,  Jae-Hoon Kim ,  Seong-Pal Lee

发明人： Byoung-Sun Lee ,  Jeong-Sook Lee ,  Hee-Sook Mo ,  Jae-Hoon Kim ,  Seong-Pal Lee

IPC分类号： B64G1/36

CPC分类号： H04B7/18519 ,  B64G1/24 ,  B64G1/242 ,  B64G3/00

摘要： Disclosed is a command planning apparatus of a low-earth orbit satellite, and a low-earth orbit satellite control system including the same. The present invention automates the process of executing the command plan for converting the satellite task schedule planned on the ground into telecommands available by the satellite in the low-earth orbit satellite control system, and automatically selects a data set established by the parameters related to the execution task of the satellite according to the mapping rule.

公开(公告)号：US08639398B2

公开(公告)日：2014-01-28

申请号：US13307358

申请日：2011-11-30

申请人： In-Jun Kim ,  Byoung-Sun Lee ,  Jae-Hoon Kim

发明人： In-Jun Kim ,  Byoung-Sun Lee ,  Jae-Hoon Kim

IPC分类号： G01C23/00

CPC分类号： H04B7/18519

摘要： An apparatus for automatically generating satellite operation procedure (SOP) parameters is provided. The apparatus includes a parameter extraction unit configured to extract one or more SOP parameters corresponding to an SOP; a transformation formula extraction unit configured to extract a transformation formula corresponding to the extracted SOP parameters; and a calculation unit configured to calculate values of the extracted SOP parameters based on property information for performing a satellite task and the extracted transformation formula.

摘要翻译： 提供一种用于自动生成卫星操作程序（SOP）参数的装置。 该装置包括：参数提取单元，被配置为提取与SOP对应的一个或多个SOP参数; 变换公式提取单元，被配置为提取与所提取的SOP参数相对应的变换公式; 以及计算单元，被配置为基于用于执行卫星任务的属性信息和所提取的变换公式来计算所提取的SOP参数的值。

公开(公告)号：US20100090889A1

公开(公告)日：2010-04-15

申请号：US12443464

申请日：2007-09-17

申请人： Yoola Hwang ,  Byoung-Sun Lee ,  Hae-Yeon Kim ,  Jae-Hoon Kim

发明人： Yoola Hwang ,  Byoung-Sun Lee ,  Hae-Yeon Kim ,  Jae-Hoon Kim

IPC分类号： G01S19/41

CPC分类号： G01S19/42 ,  G01S19/09 ,  G01S19/14 ,  G01S19/33 ,  G01S19/39

摘要： Provided are a method and system for determining a precise orbit of a LEO satellite. The method includes: estimating a precise ephemeris of a global positioning system (GPS) satellite by fitting an orbit perturbation-based GPS dynamics model to observation data of the GPS satellite received from a GPS observatory and estimating a precise ephemeris of a Galileo satellite by fitting an orbit perturbation-based Galileo dynamics model to observation data of the Galileo satellite received from a Galileo observatory; determining an initial orbit value of a LEO satellite by fitting an orbit perturbation-based LEO satellite's basic dynamics model to navigation data received from the LEO satellite; and determining the precise orbit of the LEO satellite by calculating a difference between observation values, which are calculated based on a GPS and Galileo data received from the LEO satellite, the GPS observatory and the Galileo observatory, and calculated values, which are calculated based on an orbit perturbation-based LEO satellite's dynamics model that was calculated using the initial orbit value of the LEO satellite and the precise ephemeris of the GPS and Galileo satellites. Since both the GPS and Galileo data are received and used to determine the precise orbit of a LEO satellite, more precise orbit determination can be achieved.

摘要翻译： 提供了一种用于确定LEO卫星的精确轨道的方法和系统。 该方法包括：通过将基于轨道扰动的GPS动力学模型拟合到从GPS天文台接收的GPS卫星的观测数据，估计全球定位系统（GPS）卫星的精确星历，并通过拟合估计伽利略卫星的精确星历 基于轨道扰动的伽利略动力学模型，用于从伽利略天文台收到的伽利略卫星的观测数据; 通过将基于轨道扰动的LEO卫星的基本动力学模型拟合到从LEO卫星接收的导航数据来确定LEO卫星的初始轨道值; 以及通过计算基于从LEO卫星，GPS天文台和伽利略天文台接收的GPS和伽利略数据计算的观测值之间的差异以及基于以下计算的计算值来确定LEO卫星的精确轨道： 使用LEO卫星的初始轨道值和GPS和伽利略卫星的精确星历计算的基于轨道扰动的LEO卫星动力学模型。 由于GPS和伽利略数据都被接收并用于确定LEO卫星的精确轨道，因此可以实现更精确的轨道确定。

公开(公告)号：US07542829B2

公开(公告)日：2009-06-02

申请号：US10536601

申请日：2003-09-26

申请人： Byoung-Sun Lee ,  Jeong-Sook Lee ,  Hee-Sook Mo ,  Jae-Hoon Kim ,  Seong-Pal Lee

发明人： Byoung-Sun Lee ,  Jeong-Sook Lee ,  Hee-Sook Mo ,  Jae-Hoon Kim ,  Seong-Pal Lee

IPC分类号： G05D1/00 ,  G05D3/00 ,  G06F7/00 ,  G06F17/00 ,  G06F19/00 ,  G06G7/70 ,  G01S1/00 ,  H04B7/00 ,  B64G1/00

CPC分类号： H04B7/18519 ,  B64G1/24 ,  B64G1/242 ,  B64G3/00

摘要： Disclosed is a command planning apparatus of a low-earth orbit satellite, and a low-earth orbit satellite control system including the same. The present invention automates the process of executing the command plan for converting the satellite task schedule planned on the ground into telecommands available by the satellite in the low-earth orbit satellite control system, and automatically selects a data set established by the parameters related to the execution task of the satellite according to the mapping rule.

摘要翻译： 本发明公开了一种低地球轨道卫星的指挥规划装置和包括该地球轨道卫星的低地球轨道卫星控制系统。 本发明自动执行用于将地面上计划的卫星任务进度转换为卫星在低地球轨道卫星控制系统中可用的遥控命令的命令计划的过程，并且自动选择由与地球轨道卫星控制系统相关的参数建立的数据集 卫星的执行任务根据映射规则。

公开(公告)号：US06683563B2

公开(公告)日：2004-01-27

申请号：US10194242

申请日：2002-07-15

申请人： Jeong-Sook Lee ,  Byoung-Sun Lee ,  Jae-Hoon Kim ,  Seong-Pal Lee ,  Jae-Cheol Yoon ,  Kyu-Hong Choi ,  Kyoung-Min Roh ,  Eun-Seo Park ,  Bo-Yeon Moon

发明人： Jeong-Sook Lee ,  Byoung-Sun Lee ,  Jae-Hoon Kim ,  Seong-Pal Lee ,  Jae-Cheol Yoon ,  Kyu-Hong Choi ,  Kyoung-Min Roh ,  Eun-Seo Park ,  Bo-Yeon Moon

IPC分类号： G01S502

CPC分类号： G01S19/43 ,  B64G1/1021 ,  B64G1/36 ,  G01S19/02 ,  G01S19/09 ,  G01S19/32

摘要： In a system for determining a precise orbit of a satellite, a satellite control system includes a tracking, telemetry and command module for receiving telemetry data from the satellite, tracking the satellite, and performing link to the satellite; a satellite operations sub module for extracting L1 carrier phase data by processing the telemetry data, monitoring the satellite, generating telecommand data, and controlling the satellite; and a mission analysis and planning subsystem for determining the precise orbit of the satellite using the L1 carrier phase data collected by a satellite, L1/L2 carrier phase data of the reference ground stations of the GPS satellites collected by an IGS, and a path error caused by the ionosphere of data, and analyzing and planning a mission of the satellite.

摘要翻译： 在用于确定卫星的精确轨道的系统中，卫星控制系统包括跟踪，遥测和命令模块，用于从卫星接收遥测数据，跟踪卫星并执行与卫星的连接; 卫星操作子模块，用于通过处理遥测数据，监测卫星，产生遥控数据和控制卫星来提取L1载波相位数据; 以及使用由卫星收集的L1载波相位数据来确定卫星的精确轨道的任务分析和规划子系统，由IGS收集的GPS卫星的参考地面站的L1 / L2载波相位数据和路径误差 由数据电离层引起的，并分析和规划卫星的使命。

公开(公告)号：US08902386B2

公开(公告)日：2014-12-02

申请号：US13462084

申请日：2012-05-02

申请人： Oh Jeong Kwon ,  Jae Hong Park ,  Sung-Jae Yun ,  Hyeok Jin Lee ,  Mee Hye Jung ,  Jiang Shuai ,  Kyung Hye Park ,  Jae-Hoon Kim

发明人： Oh Jeong Kwon ,  Jae Hong Park ,  Sung-Jae Yun ,  Hyeok Jin Lee ,  Mee Hye Jung ,  Jiang Shuai ,  Kyung Hye Park ,  Jae-Hoon Kim

IPC分类号： G02F1/1337 ,  G02F1/1343 ,  G02F1/1334

CPC分类号： G02F1/1337 ,  G02F1/133707 ,  G02F1/133753 ,  G02F1/133788 ,  G02F1/134309 ,  G02F2001/13345 ,  G02F2001/133742 ,  G02F2001/133757 ,  G02F2001/133761 ,  G02F2001/134318

摘要： A liquid crystal display according to an exemplary embodiment of the present invention includes a first substrate, a pixel electrode disposed on the first substrate, a first alignment layer disposed on the first substrate and the pixel electrode, a second substrate facing the first substrate, a common electrode disposed on the second substrate, a second alignment layer disposed on the second substrate and the common electrode, and a liquid crystal layer disposed between the first substrate and the second substrate, in which the common electrode has a first opening having a cross shape, an edge of the first opening protrudes beyond an edge of the pixel electrode, and the pixel electrode includes a second opening disposed adjacently to at least one of the edges of the pixel electrode.

摘要翻译： 根据本发明的示例性实施例的液晶显示器包括第一基板，设置在第一基板上的像素电极，设置在第一基板上的第一取向层和像素电极，面对第一基板的第二基板， 设置在第二基板上的公共电极，设置在第二基板和公共电极上的第二取向层，以及设置在第一基板和第二基板之间的液晶层，其中公共电极具有十字形状的第一开口 第一开口的边缘突出超过像素电极的边缘，并且像素电极包括与像素电极的至少一个边缘相邻设置的第二开口。

公开(公告)号：US08810761B2

公开(公告)日：2014-08-19

申请号：US13460667

申请日：2012-04-30

申请人： Jae Hong Park ,  Sung-Jae Yun ,  Jae-Soo Jang ,  Jun Ha Park ,  Jeong Ho Lee ,  Hyeok Jin Lee ,  Sung Hwan Hong ,  Oh Jeong Kwon ,  Jae-Hoon Kim ,  Kwang-Soo Bae

发明人： Jae Hong Park ,  Sung-Jae Yun ,  Jae-Soo Jang ,  Jun Ha Park ,  Jeong Ho Lee ,  Hyeok Jin Lee ,  Sung Hwan Hong ,  Oh Jeong Kwon ,  Jae-Hoon Kim ,  Kwang-Soo Bae

IPC分类号： G02F1/1337 ,  G02F1/1343

CPC分类号： G02F1/133707 ,  G02F1/133753 ,  G02F1/133788 ,  G02F1/13624 ,  G02F2001/133742 ,  G02F2001/133746 ,  G02F2001/133757 ,  G02F2001/134318 ,  G02F2001/134345 ,  G02F2201/122 ,  G02F2201/123

摘要： A liquid crystal display according to an exemplary embodiment of the present invention includes: a first substrate; a pixel electrode disposed on the first substrate; a first alignment layer disposed on the first substrate and the pixel electrode; a second substrate facing the first substrate; a common electrode disposed on the second substrate; a second alignment layer disposed on the second substrate and the common electrode; and a liquid crystal layer disposed between the first substrate and the second substrate, wherein the common electrode has a plurality of cutouts having a cross shape, and when viewing the first substrate and the second substrate upward, the edge of the cutout is protruded from the edge of the pixel electrode.

摘要翻译： 根据本发明的示例性实施例的液晶显示器包括：第一基板; 设置在所述第一基板上的像素电极; 设置在所述第一基板和所述像素电极上的第一取向层; 面对所述第一基板的第二基板; 设置在所述第二基板上的公共电极; 设置在所述第二基板和所述公共电极上的第二取向层; 以及设置在第一基板和第二基板之间的液晶层，其中公共电极具有多个具有十字形状的切口，并且当向上观看第一基板和第二基板时，切口的边缘从 像素电极的边缘。

公开(公告)号：USD709207S1

公开(公告)日：2014-07-15

申请号：US29441140

申请日：2012-12-31

申请人： Jae-Hoon Kim

设计人： Jae-Hoon Kim