| 运载火箭三通道调姿系统的设计和数学仿真 |
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| 引用本文： | 高玉林 狄淑月. 运载火箭三通道调姿系统的设计和数学仿真[J]. 导弹与航天运载技术, 1994, 0(4): 15-22 |
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| 作者姓名： | 高玉林 狄淑月 |
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| 作者单位： | 北京航天自动控制研究所 |
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| 摘 要： | 本文论述了运载火箭三通道大姿态的设计和数学仿真。首先建立了箭体全量，三通道运动模型，接着介绍了用多变量系统现代频域理论，进行调姿系统设计的基本思想和方法，最后以实例给出系统设计和数学仿真结果。
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| 关 键 词： | 运载火箭 姿态控制 数学模拟 |
The Design and Mathematical Simulation of the Three-axis Attitude-adjusting System of Launch Vehicle |
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| Gao Yulin, Di Shuyue. The Design and Mathematical Simulation of the Three-axis Attitude-adjusting System of Launch Vehicle[J]. Missiles and Space Vehicles, 1994, 0(4): 15-22 |
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| Authors: | Gao Yulin Di Shuyue |
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| Affiliation: | Beijing Aerospace Automatic Control Institute |
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| Abstract: | This paper describes the design and mathematical simulation of the three-axis attitude-adjusting system of launch vehicle. First, the models of launch vehicle and its three-axis motion are built, and then the basic ideology and method of designing attitude-adjusting system by modern frequency domain theory of multivariable system are presented. Finally, the results of system design and mathematical simulation of actual models are given. |
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| Keywords: | Launch vehicle Attitude control Mathematical simulation. |
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