The Experimental Vibration Analysis of Small-scale Unmanned Helicopter for Control Design

被引：0
|
作者：
Tang, Shuai [1 ]
Liu, GuoSong [1 ]
Zhang, Li [1 ]
Zhou, Bin [2 ]
机构：
[1] Army Logist Univ PLA, Chongqing 401311, Peoples R China
[2] Natl Univ Def Technol, Changsha 410073, Hunan, Peoples R China
来源：
2018 37TH CHINESE CONTROL CONFERENCE (CCC) | 2018年
关键词：
Small-scale helicopter; Vibration; Intensity; Natural frequency; Frequency spectrum;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
This paper focuses on the experimental vibration analysis of the small-scale unmanned helicopter and the methods to weaken the influence for control design. The vibration source of the small-scale helicopter and the evaluation criteria are introduced. The influence of the main blades dynamic balance on vibration is analyzed and the way to decrease is presented; based on frequency domain analysis technology, the influence of the main rotor speed is well-analyzed and the method to optimize the rotor speed is proposed. The experimental results show that the analysis and the methods are effective and suitable for vibration reduction.
引用
收藏
页码：9831 / 9836
页数：6
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