| 带有飞行控制系统飞机的伺服弹性试验研究 |
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| 引用本文： | 章俊杰,杨超.带有飞行控制系统飞机的伺服弹性试验研究[J].北京航空航天大学学报,2003,29(11):998-1000. |
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| 作者姓名： | 章俊杰 杨超 |
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| 作者单位： | 北京航空航天大学 航空科学与工程学院, 北京 100083 |
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| 摘 要： | 以一架具有飞行控制系统的飞机为对象,开展了伺服弹性(结构模态耦合)试验研究,旨在揭示该飞机的伺服弹性稳定性本质.同时,阐述了结构模态耦合试验的方法和原理,给出了典型状态的试验结果,并与计算分析结果进行了比较.说明该试验方法是可行的.
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| 关 键 词： | 伺服系统 试验 稳定性 |
| 文章编号： | 1001-5965(2003)11-0998-03 |
| 收稿时间： | 2003-07-05 |
Servo-elasticity test of an aircraft with the flight control system |
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| Zhang Junjie,Yang Chao.Servo-elasticity test of an aircraft with the flight control system[J].Journal of Beijing University of Aeronautics and Astronautics,2003,29(11):998-1000. |
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| Authors: | Zhang Junjie Yang Chao |
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| Institution: | School of Aeronautics Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China |
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| Abstract: | To discover the servo-elasticity stability nature of an aircraft equipped with a flight control system, some active-control-system/structural dynamics interaction tests on it have been performed. The test principle and test method was described. Some typical test results have been presented and compared with the calculated results. The test method is reasonable. |
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| Keywords: | servo systems test stability |
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