卫星单轴姿态控制全物理仿真平台动态测试系统设计  

Design of Dynamic Test System for Satellite Uniaxial Attitude Full Physical Simulation Platform

作　　者：安若铭[1] 邢坤鹏 荆武兴[1] An Ruoming;Xing Kunpeng;Jing Wuxing(School of Astronautics,Harbin Institute of Technology,Harbin,150001,China)

机构地区：[1]哈尔滨工业大学航天学院,黑龙江哈尔滨150001

出　　处：《中国现代教育装备》2021年第19期18-21,共4页China Modern Educational Equipment

摘　　要：卫星单轴姿态控制全物理仿真平台的性能优劣直接影响着对其是否具有天地一致性的评判,故对姿态物理仿真平台的测试具有重要的实际意义。针对这一需求,通过处理仿真平台的转角数据,基于数据库和LabVIEW搭建了卫星单轴姿态控制全物理仿真平台动态测试系统。该测试系统可采集角度数据、计算数据误差,并具有波形分析、数据存储调用和实验报告打印等功能。在仿真平台上的应用验证了该测试系统的有效性。The performance of the satellite unizxial attitude physical simulation platform directly affects the evaluation of its consistency between heaven and earth,so there is important practical significance for the test of the attitude physical simulation platform.In this paper,by processing the Angle data of simulation platform,a satellite attitude control performance dynamic test system is built based on the database and Labview.This test system not only can collect angle data,calculate data errors,but also can analysis waveform,storage and call data,and print experiment report.The application on the simulation platform verifies the effectiveness of the test system.

关 键 词：卫星姿态控制仿真 数据库 转角测试系统 LABVIEW 

分 类 号：V448.22[航空宇航科学与技术—飞行器设计] V416.8