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SATELLITE SIMULATION SYSTEM USING COMPONENT-BASED SATELLITE MODELING

机译：基于组件的卫星建模的卫星仿真系统

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摘要

PPROBLEM TO BE SOLVED: To form a component-based model by separating data dependent on each satellite and characteristics of a modeling object, and to perform simulation by running the model and scheduling and time-managing a process of constituent elements. PSOLUTION: The satellite simulation system includes: a user interface unit for receiving simulation control commands and data and a parameter required for simulation from a user; a satellite model unit for individually storing information dependent on the satellite, characteristics of the simulation object model and parameter information based on the characteristics, and performing simulation upon receipt of simulation control commands; and a simulation kernel unit for creating a schedule control command for the simulation control of the satellite model unit, the onboard simulation unit and the external interface unit by the control command receiving from the user interface unit, performing control and collecting and managing simulation results. PCOPYRIGHT: (C)2007,JPO&INPIT

机译：

要解决的问题：通过分离依赖于每颗卫星和建模对象特征的数据来形成基于组件的模型，并通过运行模型并调度和时间管理组成元素的过程来执行仿真。解决方案：卫星仿真系统包括：用户接口单元，用于从用户接收仿真控制命令和数据以及仿真所需的参数;卫星模型单元，用于分别存储与卫星有关的信息，模拟对象模型的特征和基于该特征的参数信息，并在接收到模拟控制命令时进行模拟。模拟内核单元，用于通过从用户接口单元接收控制命令来创建用于对卫星模型单元，机载模拟单元和外部接口单元进行模拟控制的调度控制命令，进行控制以及收集和管理模拟结果。

版权：（C）2007，日本特许厅＆INPIT 展开▼

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公开/公告号JP2007157106A

专利类型
公开/公告日2007-06-21

原文格式PDF
申请/专利权人 KOREA ELECTRONICS TELECOMMUN;
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申请/专利号JP20060131898
发明设计人 LEE SANG-UK;JUNG OK-CHUL;JEONG SEONG-KYUN;KIM JE FUN;
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申请日2006-05-10
分类号G06F19;B64G1/10;G05D1/08;
国家 JP
入库时间 2022-08-21 21:14:23

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