| 共轴式小型直升机操纵系统动态特性分析研究 |
| |
| 引用本文： | 冯亚昌,李胜军.共轴式小型直升机操纵系统动态特性分析研究[J].北京航空航天大学学报,2003,29(5):410-414. |
| |
| 作者姓名： | 冯亚昌 李胜军 |
| |
| 作者单位： | 北京航空航天大学 自动化科学与电气工程学院 |
| |
| 摘 要： | 对某共轴式小型遥控直升机纵向系统建立了工程实用的数学模型,分析研究了该系 统动态特性和参数变化对其动特性的影响.通过与试验、试飞比较,证明该模型是正确的、 可信的、其精度符合工程要求.
|
| 关 键 词： | 直升机 数学模型 动态性能 |
| 文章编号： | 1001-5965(2003)05-0410-05 |
| 收稿时间： | 2002-02-27 |
| 修稿时间： | 2002年2月27日 |
Analysis and Study Dynamical Characteristics of Control System of Small Coaxial Helicopter |
| |
| Feng Yachang\ Li Shengjun.Analysis and Study Dynamical Characteristics of Control System of Small Coaxial Helicopter[J].Journal of Beijing University of Aeronautics and Astronautics,2003,29(5):410-414. |
| |
| Authors: | Feng Yachang\ Li Shengjun |
| |
| Institution: | School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics |
| |
| Abstract: | Not only practical mathematics model of longilndinal system was established for small coaxial helicopter remotely, but also the dynamical characteristics and the influence of parameter change were analyzed. By experiment and flying test data, the model is proved to be correct, belivable, and its precision corresponds with the demand of engineering. |
| |
| Keywords: | helicopters mathematical models dynamic properties |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
| 点击此处可从《北京航空航天大学学报》浏览原始摘要信息 |
| 点击此处可从《北京航空航天大学学报》下载免费的PDF全文 |
