公开(公告)号：KR100766000B1

公开(公告)日：2007-10-12

申请号：KR1020060128495

申请日：2006-12-15

Applicant: 한국항공우주연구원

Inventor： 김용복 ,  이승우 ,  오시환 ,  이선호 ,  임조령 ,  용기력

IPC: B64G1/24

CPC classification number: B64G1/36 ,  G05D1/0883

Abstract: An integrated verification system for controlling a satellite attitude is provided to improve the efficiency of control logic verification by displaying a geometric appearance of a satellite in a three-dimensional space. An integrated verification system comprises a satellite dynamic simulator(10), a remote interface device(20), an embedded computer simulator(30), a satellite attitude control three-dimensional graphic visual device(40), a star simulator(50) and a host PC(60). The satellite dynamic simulator(10) includes a hardware having a commercial board and a custom board, and a software. The remote interface device(20) collects information on satellite attitude from an attitude control sensor, and sends the information to an attitude control logic.

Abstract translation: 提供用于控制卫星姿态的综合验证系统，以通过在三维空间中显示卫星的几何外观来提高控制逻辑验证的效率。 集成验证系统包括卫星动态模拟器（10），远程接口设备（20），嵌入式计算机模拟器（30），卫星姿态控制三维图形视觉设备（40），星型模拟器（50）和 主机PC（60）。 卫星动态模拟器（10）包括具有商业板和定制板的硬件以及软件。 远程接口装置（20）从姿态控制传感器收集关于卫星姿态的信息，并将该信息发送到姿态控制逻辑。