| 3自由度直升飞机控制系统设计 |
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| 引用本文： | 姜增如,李延博.3自由度直升飞机控制系统设计[J].实验技术与管理,2007,24(1):52-56. |
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| 作者姓名： | 姜增如 李延博 |
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| 作者单位： | 北京理工大学,信息科学技术学院自动控制系,北京,100081 |
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| 摘 要： | 该试验讨论了针对固高科技有限公司提供的3自由度直升飞机试验装置的一种非线性控制算法。文章首先分析了该系统的结构与特点,然后详细研究并建立了针对铰链装置的动力学模型,接着设计并实现了基于上述模型的直接转矩控制算法。最后文章通过引用实验结果演示了该控制算法的控制效果。
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| 关 键 词： | 非线性 铰链动力学模型 直接转矩控制 直升飞机 |
| 文章编号： | 1002-4956（2007）01-0052-05 |
| 收稿时间： | 2006-04-14 |
| 修稿时间： | 2006-12-04 |
A new control method of a 3- DOF- helicopter device based on digital control |
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| JIANG Zeng-ru,LI Yan-bo.A new control method of a 3- DOF- helicopter device based on digital control[J].Experimental Technology and Management,2007,24(1):52-56. |
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| Authors: | JIANG Zeng-ru LI Yan-bo |
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| Institution: | Department of Automatic Control, School of Information Science and Technology, Beijing Institute of Technology, Beijing 100081, China |
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| Abstract: | In order to control a non-linear and highly coupled 3 DOF helicopter device,a new method of modeling is proposed.The advantage of this method is that it can precisely describe the non-linear and highly coupled system.Then a control method according to that is presented.The experiment conducted on simulator proved high efficiency and high precision of this method and demonstrated the good performance as the result of this new method. |
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| Keywords: | non-linear hinge dynamics model direct torch control helicopter |
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