| 旋转火箭的姿态控制设计方法 |
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| 引用本文： | 刘继忠,吴长才.旋转火箭的姿态控制设计方法[J].航天控制,1997(4). |
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| 作者姓名： | 刘继忠 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： | 介绍了非对称旋转火箭姿态控制的方案、原理。并且利用角速度控制和最佳程序控制，分析了大滚动角消旋的稳定性。数值仿真结果显示了所设计的控制算法的有效性。
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| 关 键 词： | 姿态控制 起旋 消旋 失控 火箭 |
The Methods of Attitude Control Design for Spinning Rocket |
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| Liu Jizhong, Wu Changcai.The Methods of Attitude Control Design for Spinning Rocket[J].Aerospace Control,1997(4). |
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| Authors: | Liu Jizhong Wu Changcai |
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| Institution: | Beiing Aerospace Automatic Control Institute 100854 |
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| Abstract: | The attitude control scheme and principle for a spinning unsymmetrical rocket areintroduced. With the application of angular relority control and optimal program control,the stability of large - roll - angle despun is analyzed. Numerical simulation results showthat the control algorithm designed in this paper is effective. |
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| Keywords: | Attitude control Spinning Despun Runaway Rocket |
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