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    • 1. 发明授权
    • Apparatus for determining diameter of parabolic antenna and method therefor
    • 用于确定抛物面天线直径的装置及其方法
    • US07653501B2
    • 2010-01-26
    • US12088461
    • 2005-12-26
    • Jeom-hun LeeJae-Hoon KimHo-Jin Lee
    • Jeom-hun LeeJae-Hoon KimHo-Jin Lee
    • G01R23/00
    • G01B21/10H01Q19/132
    • Provided are an apparatus and method for determining a diameter of a reflector antenna. The apparatus includes a setting unit for setting up electrical characteristic values of the reflector antenna upon receipt thereof from outside, a parameter input unit for receiving a frequency, an antenna diameter variable value, antenna efficiency, Edge Taper (ET), and an Edge Of Coverage (EOC) angle as parameters for each of multiple frequencies to be accommodated in the reflector antenna, a graph generator for generating, on one rectangular coordinate, a graph representing the relationship between an antenna diameter and EOC directivity with respect to the EOC angle based on the parameters for each frequency received through the parameter input unit, an antenna diameter determination unit for determining an antenna diameter that simultaneously meets the preset EOC directivities for the frequencies to be accommodated in the reflector antenna by using the graph generated by the graph generation unit, and a graph output unit for mapping and outputting the graph generated by the graph generation unit on one rectangular coordinate with an antenna diameter axis and an EOC directivity axis to thereby represent the antenna diameter determined by the antenna diameter determination unit on the graph.
    • 提供了一种用于确定反射器天线的直径的装置和方法。 该装置包括:设置单元,用于在从外部接收反射器天线时设置反射器天线的电特性值,用于接收频率的参数输入单元,天线直径可变值,天线效率,边缘锥度(ET) 覆盖(EOC)角度作为要容纳在反射器天线中的多个频率中的每一个的参数,图形生成器,用于在一个矩形坐标上生成表示相对于基于EOC角度的天线直径和EOC方向性之间的关系的曲线图 关于通过参数输入单元接收的每个频率的参数,天线直径确定单元,用于通过使用由图形生成单元生成的图形来确定同时满足反射天线中容纳的频率的预设EOC方向性的天线直径 以及用于映射和输出由该图形生成的图形的图形输出单元 生成单元,其具有天线直径轴和EOC方向轴的一个矩形坐标,从而表示由图中天线直径确定单元确定的天线直径。
    • 2. 发明申请
    • Apparatus for Determining Diameter of Parabolic Antenna and Method Therefor
    • 用于确定抛物线天线直径的装置及其方法
    • US20080249739A1
    • 2008-10-09
    • US12088461
    • 2005-12-26
    • Jeom-Hun LeeJae-Hoon KimHo-Jin Lee
    • Jeom-Hun LeeJae-Hoon KimHo-Jin Lee
    • G01B21/10
    • G01B21/10H01Q19/132
    • Provided are an apparatus and method for determining a diameter of a reflector antenna. The apparatus includes a setting unit for setting up electrical characteristic values of the reflector antenna upon receipt thereof from outside, a parameter input unit for receiving a frequency, an antenna diameter variable value, antenna efficiency, Edge Taper (ET), and an Edge Of Coverage (EOC) angle as parameters for each of multiple frequencies to be accommodated in the reflector antenna, a graph generator for generating, on one rectangular coordinate, a graph representing the relationship between an antenna diameter and EOC directivity with respect to the EOC angle based on the parameters for each frequency received through the parameter input unit, an antenna diameter determination unit for determining an antenna diameter that simultaneously meets the preset EOC directivities for the frequencies to be accommodated in the reflector antenna by using the graph generated by the graph generation unit, and a graph output unit for mapping and outputting the graph generated by the graph generation unit on one rectangular coordinate with an antenna diameter axis and an EOC directivity axis to thereby represent the antenna diameter determined by the antenna diameter determination unit on the graph.
    • 提供了一种用于确定反射器天线的直径的装置和方法。 该装置包括:设置单元,用于在从外部接收反射器天线时设置反射器天线的电特性值,用于接收频率的参数输入单元,天线直径可变值,天线效率,边缘锥度(ET) 覆盖(EOC)角度作为要容纳在反射器天线中的多个频率中的每一个的参数,图形生成器,用于在一个矩形坐标上生成表示相对于基于EOC角度的天线直径和EOC方向性之间的关系的曲线图 关于通过参数输入单元接收的每个频率的参数,天线直径确定单元,用于通过使用由图形生成单元生成的图形来确定同时满足反射天线中容纳的频率的预设EOC方向性的天线直径 以及用于映射和输出由该图形生成的图形的图形输出单元 生成单元,其具有天线直径轴和EOC方向轴的一个矩形坐标,从而表示由图中天线直径确定单元确定的天线直径。
    • 3. 发明申请
    • Hybrid type satellite simulation system and method thereof
    • 混合型卫星仿真系统及其方法
    • US20060100846A1
    • 2006-05-11
    • US11182133
    • 2005-07-14
    • Sang-Uk LeeJae-Hoon KimHo-Jin LeeSeong-Pal Lee
    • Sang-Uk LeeJae-Hoon KimHo-Jin LeeSeong-Pal Lee
    • G06F9/45
    • B64G7/00B64G1/24H04L67/38
    • A hybrid-type satellite simulation system and a method thereof are disclosed. The system includes: a satellite modeling unit including a satellite model and a software model having flight dynamics and space environment data; a satellite operation unit for generating a telecommand, transmitting the telecommand to the satellite simulation system, receiving simulation result as a telemetry, analyzing the simulation result and displaying the analyzed result; a simulator kernel for managing and controlling the satellite simulation system; a TCP/IP interface processing unit for performing an interface function of TCP/IP level between the simulator kernel and a satellite onboard computer; an onboard computer interface processing unit for performing an interface function between the satellite onboard computer and the TCP/IP interface processing unit; and a satellite onboard computer including flight software for controlling a satellite.
    • 公开了一种混合型卫星仿真系统及其方法。 该系统包括:包括卫星模型和具有飞行动力学和空间环境数据的软件模型的卫星建模单元; 用于产生遥控的卫星操作单元,向卫星仿真系统发送遥控信号,接收模拟结果作为遥测,分析仿真结果并显示分析结果; 用于管理和控制卫星仿真系统的模拟器内核; TCP / IP接口处理单元,用于在模拟器内核和机载计算机之间执行TCP / IP级别的接口功能; 车载计算机接口处理单元,用于在卫星机载计算机和TCP / IP接口处理单元之间执行接口功能; 以及包含用于控制卫星的飞行软件的卫星机载计算机。