宇航计测技术
• 论文 • 下一篇
王小三1;刘云平1;倪怀生1;张宁2
出版日期:
发布日期:
作者简介:
WANG Xiao-san1;LIU Yun-ping1;NI Huai-sheng1;ZHANG Ning2
Online:
Published:
摘要: 对转动惯量测量的研究情况作了综述,对三线摆法、扭摆法、落体法等转动惯量测量方法的测量原理及其优缺点进行了总结,介绍了针对以上缺点的一种新的测量方法,预测该方法将代表转动惯量测量的发展方向。
关键词: 转动惯量, 研究进展, 扭摆法, 空气阻尼
Abstract: A review on the measurement research of the moment of inertia is carried out. The principles of some current measurement methods of the moment of inertia, such as the trilinear pendulum method, the torsion pendulum method and the falling body method, are summarized as well as their advantages and disadvantages. A new method aimed at these disadvantages is introduced, which is prospected to be a development direction for the measurement of the moment of inertia.
Key words: Moment of inertia, Research progress, Torsion pendulum method, Air damping
王小三;刘云平;倪怀生;张宁. 转动惯量测量研究的进展及展望[J]. 宇航计测技术, doi: 10.12060/j.issn.1000-7202.2019.02.01.
WANG Xiao-san;LIU Yun-ping;NI Huai-sheng;ZHANG Ning. Progress and Prospects for the Measurement Research on the Moment of Inertia[J]. JOURNAL OF ASTRONAUTIC METROLOGY AND MEASUREMENT, doi: 10.12060/j.issn.1000-7202.2019.02.01.
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.1000-7202.2019.02.01
http://www.yhjcjs.com.cn/CN/Y2019/V39/I2/1