| 3—自由度直升机模型的分析与控制器设计 |
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| 引用本文： | 胡睿,鲍俊卿,饶祺.3—自由度直升机模型的分析与控制器设计[J].科技广场,2012(5):100-102. |
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| 作者姓名： | 胡睿 鲍俊卿 饶祺 |
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| 作者单位： | 中航工业洪都集团650所,江西南昌,330024 |
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| 摘 要： | 本文以3—自由度直升飞机系统为模拟平台,针对其线性化模型,采用了LQR方法对直升机控制器进行设计以提高系统的性能,针对该方法加入了内模,以增强系统的跟踪能力和抗干扰能力。
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| 关 键 词： | 3—自由度直升飞机 线性化模型 LQR |
The Controller Design and Analysis of 3-DOC Helicopter Model |
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| Hu Rui Bao Junqing Rao Qi.The Controller Design and Analysis of 3-DOC Helicopter Model[J].Science Mosaic,2012(5):100-102. |
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| Authors: | Hu Rui Bao Junqing Rao Qi |
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| Institution: | Hu Rui Bao Junqing Rao Qi(650th Institute of Hongdu Aviation Group,Aviation Industry Corporation of China,Jiangxi Nanchang 330024) |
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| Abstract: | In this paper,3-DOC helicopter system is applied as a simulator platform.According to its characteristic of linear model,a method of LQR is adopted to design the helicopter controller to improve the performance of the system.In order to improve the tracking and anti-jamming capabilities of the system,an internal model is used to this method. |
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| Keywords: | 3-DOC Helicopter Model Linear Model LQR |
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