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| 小型无人驾驶直升机动力学模型辨识仿真研究 | |
| 引用本文： | 陈文兵,李从利,陆文骏,葛运建.小型无人驾驶直升机动力学模型辨识仿真研究[J].自动化与仪表,2010,25(3):7-9,58. |
| 作者姓名： | 陈文兵 李从利 陆文骏 葛运建 |
| 作者单位： | 1. 解放军炮兵学院,合肥,230031;中国科学院合肥智能机械研究所,合肥,230031 2. 解放军炮兵学院,合肥,230031 3. 中国科学院合肥智能机械研究所,合肥,230031 |
| 摘 要： | 获得足够精确的动力学模型．对于小型无人驾驶直升机这种MIMO控制系统研究具有重要的意义。文中研究了直升机模型辨识方法，将子空间辨识算法运用于直升机动力学模型的辨识，并对模型直升机的垂直——偏航耦舍运动方程进行了辨识，得到了较为精确的结果,通过和PEM算法进行比较，显示该算法适合模型直升机系统辨识。 |
| 关 键 词： | 子空间 系统辨识 无人直升机 多输入多输出 预报误差方法 |
Identification and Simulation of a Small-scale Unmanned Helicopter Dynamics |
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| CHEN Wen-bing,LI Cong-li,LU Wen-jun,GE Yun-jian.Identification and Simulation of a Small-scale Unmanned Helicopter Dynamics[J].Automation and Instrumentation,2010,25(3):7-9,58. | |
| Authors: | CHEN Wen-bing LI Cong-li LU Wen-jun GE Yun-jian |
| Affiliation: | CHEN Wen-bing1,2,LI Cong-li1,LU Wen-jun1,GE Yun-jian2(1.Artillery Academe,P.L A,Hefei 230031,China,2.Hefei Institute of Intelligent Machines,Chinese Academy of Sciences,China) |
| Abstract: | It is significant for the control system of small-scale unmanned helicopter that the dynamic model must be accurate and simple enough.This paper researched the identification methods of model helicopter,and describes the subspace identification method to identified a small-scale helicopter dynamics which is in vertical-yaw coupled state.By compared the result of this method with that of PEM,it shows that subspace method is suitable for the dynamic identification of a small-scale helicopter. |
| Keywords: | subspace system identification unmanned helicopter MIMO PEM |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |