| 运载火箭姿控系统数学仿真软件设计 |
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| 引用本文： | 吴长才.运载火箭姿控系统数学仿真软件设计[J].航天控制,1997(3). |
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| 作者姓名： | 吴长才 |
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| 作者单位： | 北京航天自动控制研究所!100854 |
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| 摘 要： | 分析了运载火箭姿控系统箭体动力学运动方程和控制器数学模型特点，并且按照校正网络、执行机构、箭体方程、测量方程顺序设计数学仿真软件。该软件能方便地完成姿控系统数学仿真任务。由于采用三级模块结构设计，该软件具有结构清晰、层次分明、调试简单、功能齐全、使用方便等明显优点。
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| 关 键 词： | 模型 软件设计 数学仿真 姿态控制系统 运载火箭 |
Mathematical Simulation Software Design of Launch Vehicle Attitude Control System |
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| Wu Changcai.Mathematical Simulation Software Design of Launch Vehicle Attitude Control System[J].Aerospace Control,1997(3). |
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| Authors: | Wu Changcai |
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| Institution: | Beijing Aerospace Automatic Control Institute 100854 |
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| Abstract: | the features of rocket body dynamic motion equations and mathematical model of consroller of launch whicle attitude control system are analyzed and a mathematical simulation software is designed in sequence of correction network, actuating machanism ,rocket body equation and measuring equation. This software can accomplish mathematical simulation of attitude consrol system conveniently and as it adopts a 3 - level module structure it has many obvious advantages such as clear structure, distict lager, easy debugging , complete function , convenisnt operation etc. |
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| Keywords: | Model Software design Mathematical simulation Attitude control system Launch vehicle |
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