| 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].适用技术之窗,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 & Technology Plaza,2012(5):100-102. |
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| Authors: | Hu Rui Bao Junqing Rao Qi |
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| Affiliation: | 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 charac- teristic 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 mode/is used to this method. |
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| Keywords: | 3-DOC Helicopter Model Linear Model LQR |
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