| 基于模型参考逆方法的鲁棒控制律设计研究 |
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| 引用本文： | 陈永亮,沈宏良.基于模型参考逆方法的鲁棒控制律设计研究[J].飞行力学,2010,28(6). |
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| 作者姓名： | 陈永亮 沈宏良 |
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| 作者单位： | 南京航空航天大学航空宇航学院,江苏,南京,210016 |
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| 基金项目： | 航空科学基金(2009ZA52015); 南京航空航天大学引进人才科研启动基金资助 |
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| 摘 要： | 模型参考逆方法是一种通过对参考模型求逆来进行控制的鲁棒控制方法。基于该方法设计了某型高机动战斗机俯仰姿态鲁棒控制律。在相同控制律下,对系统参数变化、外部输入扰动及不同输入信号情况进行了数值仿真。仿真结果表明,所设计的控制律不仅简单,易于实现,而且有很强的鲁棒性和指令跟踪性能。
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| 关 键 词： | 鲁棒控制 逆系统 模型参考控制 |
Research on robust control law design based on method of model reference inverse |
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| CHEN Yong-liang,SHEN Hong-liang.Research on robust control law design based on method of model reference inverse[J].Flight Dynamics,2010,28(6). |
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| Authors: | CHEN Yong-liang SHEN Hong-liang |
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| Institution: | CHEN Yong-liang,SHEN Hong-liang(College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China) |
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| Abstract: | The method of model reference inverse is a robust control law design means by the inversion of the reference model.Based on this method,a pitch attitude robust control law was designed for a high maneuver fighter.Then a lot of simulations were performed with the system parameter variables in a big range,external input disturbances and different type input signals under the same control law designed in this paper.It is shown that the control law designed via this method is very simple and practical,and it ha... |
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| Keywords: | robust control inverse system model reference control |
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