宇航计测技术
• 论文 • 上一篇 下一篇
朱文来1;葛峰1
出版日期:
发布日期:
作者简介:
ZHU Wen-lai1;GE Feng1
Online:
Published:
摘要: 简述了陀螺减振结构与原理,通过采用有限元方法对无人直升机陀螺减振结构的减振效果进行了仿真研究,经分析陀螺减振结构的悬臂尺寸是影响减振性能的重要因素,为后续机械结构振动研究提供了一种有效的分析方法。
关键词: 陀螺仪, 结构振动, 有限元法, 模拟
Abstract: The structure and principle of the gyro vibration are described, by using the finite element method,the damping effect of unmanned helicopter gyro vibration is studied. By analyzing,the cantilever size of gyro damping structure is an important factor to affect the damping properties.That provides an effective analyzing method for subsequent mechanical structure vibration study.
Key words: Gyroscope, Structural vibration, Finite element method, Simulation
朱文来;葛峰. 无人直升机陀螺减振的仿真与分析[J]. 宇航计测技术, doi: 10.12060/j.issn.1000-7202.2014.02.09.
ZHU Wen-lai;GE Feng. Simulation and Analysis of Unmanned Helicopter Gyro Vibration[J]. JOURNAL OF ASTRONAUTIC METROLOGY AND MEASUREMENT, doi: 10.12060/j.issn.1000-7202.2014.02.09.
0 / / 推荐
导出引用管理器 EndNote|Ris|BibTeX
链接本文: http://www.yhjcjs.com.cn/CN/10.12060/j.issn.1000-7202.2014.02.09
http://www.yhjcjs.com.cn/CN/Y2014/V34/I2/34