| CCV飞机纵向解耦控制律的研究 |
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| 引用本文： | 李勇,熊海泉.CCV飞机纵向解耦控制律的研究[J].飞行力学,1992,10(3):16-26. |
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| 作者姓名： | 李勇 熊海泉 |
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| 作者单位： | 南京航空学院，南京航空学院 |
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| 摘 要： | 本文应用多输入、多输出跟踪模型法,对CCV型飞机纵向飞行控制系统的解耦控制律问题进行了研究。并以某型飞机为例,说明如何应用该方法确定三种纵向直接力模态的动态解耦控制律。
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| 关 键 词： | 主动控制技术 解耦控制律 飞机 |
AN INVESTIGATION OF A LONGITUDINAL DECOUPLING CONTROL LAW FOR A CCV TYPE AIRCRAFT |
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| Li Yong,Xiong Haiquan.AN INVESTIGATION OF A LONGITUDINAL DECOUPLING CONTROL LAW FOR A CCV TYPE AIRCRAFT[J].Flight Dynamics,1992,10(3):16-26. |
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| Authors: | Li Yong Xiong Haiquan |
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| Institution: | Nanjing Aeronautical Institute |
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| Abstract: | The multiple-input and multiple-output model following method is applied to the analysis of the longitudinal decoupling control law for a CCV type aircraft. The procedure to determine dynamical decoupling control laws is illustrated throught numerical examples for a CCV-type flighter aircraft while performing three longitudinal direct force control maneuvers. |
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| Keywords: | Active control technique Direct force control Decoupling control law Model following method |
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