模块化航天器姿态控制系统仿真研究Simulation research on attitude control system for modular spacecraft
贺广松,李新洪,王谦,张治彬,安继萍
摘要(Abstract)：
以快速响应为背景,对模块化航天器姿态控制系统进行研究。首先建立集成干扰力矩、姿态运动学、姿态动力学、控制律及飞轮、推力器两种执行机构的Simulink模型,然后应用实时仿真机对模型进行仿真。结果表明:不同执行机构的姿态控制系统能够完成对卫星姿态的实时控制并且在进行姿态调整时各有优势,最后以实时仿真机为基础设计了模块化航天器显示系统,实现了模块化航天器分系统状态和运行场景可视化。
关键词(KeyWords)： 模块化航天器;姿态控制;Simulink;执行机构;显示系统;可视化
基金项目(Foundation):
作者(Author): 贺广松,李新洪,王谦,张治彬,安继萍
DOI: 10.16652/j.issn.1004-373x.2018.18.030
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