中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
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Root-soil interface friction jointly amplified by high root density and shear deflection 期刊论文  OAI收割
CANADIAN GEOTECHNICAL JOURNAL, 2025, 卷号: 62, 页码: 17
作者:  
Lv, Ming;  Song, Dongri;  Ni, Junjun
  |  收藏  |  浏览/下载:17/0  |  提交时间:2025/04/11
Extending Gibbons-Werner method to bound orbits of massive particles 期刊论文  OAI收割
PHYSICAL REVIEW D, 2023, 卷号: 107, 期号: 10, 页码: 104046
作者:  
Huang, Yang;  Sun, Bing;  Cao, Zhoujian
  |  收藏  |  浏览/下载:22/0  |  提交时间:2023/12/07
Influence of deflection angles on flow behaviours in open-channel bends 期刊论文  OAI收割
JOURNAL OF MOUNTAIN SCIENCE, 2018, 卷号: 15, 期号: 10, 页码: 2292-2306
作者:  
Li Bing-dong;  Zhang Xin-hua;  Tang Han-song;  Tsubaki, Ryota
  |  收藏  |  浏览/下载:15/0  |  提交时间:2020/10/26
Deflection angle detecting system for the large-angle and high-linearity fast steering mirror using quadrant detector 期刊论文  OAI收割
Optical Engineering, 2018, 卷号: 57, 期号: 2, 页码: 9
作者:  
Ni, Y. X.;  Wu, J. B.;  San, X. G.;  Gao, S. J.;  Ding, S. H.
  |  收藏  |  浏览/下载:29/0  |  提交时间:2019/09/17
A Compact Low Energy Electron Microscope for Surface Analysis 期刊论文  OAI收割
chinese journal of chemical physics, 2013, 卷号: 26, 期号: 4, 页码: 369-373
作者:  
Zhang, Guan-hua;  Sun, Ju-long;  Jin, Yan-ling;  Zang, Kan;  Guo, Fang-zhun
收藏  |  浏览/下载:32/0  |  提交时间:2013/10/11
The aircraft autopilot design of parameters changing in a wide range (EI CONFERENCE) 会议论文  OAI收割
2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China
Zhen D.; Yue Z.
收藏  |  浏览/下载:30/0  |  提交时间:2013/03/25
Autopilot is an important part of aircraft  Under the action of the disturbance torque  for the flight parameters of aircraft Changing in a wide range  the range was about 16km  on the basic of analyzing the typical trajectory  the max height was about 5100m  the trajectory of feature points were selected  the deviation of lateral was about 12m  taking pitch control loop for example  the maximum angle of attack was about 3.6  a sub- PID autopilot was designed using classical control theory  the maximum elevator deflection was less than 5  using single-mode Transient suppression method  the maximum aileron deflection was less than 2  the overload due to control surface transition deflection was avoided when control parameters changing  the maximum roll was less than 5  the verification was done by non-linear simulation. The result showed that: the phase margin of autopilot was greater than 30  the response of overload can accurately track the given overload instruction. An autopilot design method of aircraft of parameter changes in a wide range was provided. 2011 IEEE.  the bandwidth was more than 14rad / s  the settling time was less than 0.7s  the maximum overshoot was 23.3%