| 引用本文: | 孙志兵,戴金海.运载火箭姿控系统三通道Simulink建模与仿真分析.[J].国防科技大学学报,2004,26(3):20-23.[点击复制] |
| SUN Zhibing,DAI Jinhai.Simulink Modeling & Simulation Analysis of the Attitude Control System on Three-channel of the Launch Vehicle[J].Journal of National University of Defense Technology,2004,26(3):20-23[点击复制] |
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| 运载火箭姿控系统三通道Simulink建模与仿真分析 |
| 孙志兵, 戴金海 |
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(国防科技大学 航天与材料工程学院，湖南 长沙 410073)
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| 摘要: |
| 以某运载火箭为例，介绍了将姿控系统数学模型转化为Simulink三通道仿真模型的方法和过程；在仿真过程中涉及到时变系数的瞬时时间固化法，分析由此引起的计算数据局部振荡，并提出解决办法；分析了用Simulink为该大型系统建模时所遇到的代数循环问题，并加以解决。 |
| 关键词: 运载火箭 系统仿真 Simulink 数据振荡 代数循环 |
| DOI： |
| 投稿日期：2003-11-29 |
| 基金项目:国家部委基金资助项目 |
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| Simulink Modeling & Simulation Analysis of the Attitude Control System on Three-channel of the Launch Vehicle |
| SUN Zhibing, DAI Jinhai |
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(College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China)
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| Abstract: |
| Exampled by a certain launch vehicle, the modeling method and modelingprocess with Simulink to mathematicalsimulation on three-channel for the vehicle attitude control system are described.The problem of the local surge of the calculated data due to the so-called freeze time method during the simulation process is analyzed and the resolvent is given. Algebraic loop problem encounteredinSimulinkmodeling of this large scale system is discussed and the resolvent is given. |
| Keywords: launch vehicle system simulation Simulink data surge algebraic loop |
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