| 空面导弹模型参考变结构控制器设计 |
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| 引用本文： | 樊冲.空面导弹模型参考变结构控制器设计[J].科学技术与工程,2010,10(13). |
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| 作者姓名： | 樊冲 |
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| 作者单位： | 西北工业大学航天学院,西安,710072 |
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| 摘 要： | 以空面导弹为对象,选择一种可行的参考模型,设计了俯仰回路的模型参考变结构控制器,以适应空面导弹全飞行弹道的姿态要求。最后给出六自由度仿真结果,并对仿真结果进行分析,验证了所提出方法的正确性和有效性。
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| 关 键 词： | 变结构控制 模型参考 六自由度仿真 |
| 收稿时间： | 2010/1/15 0:00:00 |
| 修稿时间： | 1/21/2010 8:51:34 PM |
Design of Model Reference Variable Structure Control in Air-to-Surface Missile |
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| fanchong.Design of Model Reference Variable Structure Control in Air-to-Surface Missile[J].Science Technology and Engineering,2010,10(13). |
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| Authors: | fanchong |
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| Abstract: | Took the air-to-surface missile as an object,chose a feasible reference model,and designed a model reference variable structure control system of the pith channel,the attitude on the whole flight trajectory of the air-to-surface missile is adapt.Six-degree of freedom simulation is given and the result is analysed.The result proves the effectiveness of the designed method. |
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| Keywords: | variable structure control reference model six-degree of freedom simulation |
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