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• 国家空间科学中心 [1]
• 武汉岩土力学研究所 [1]

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• 期刊论文 [6]
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浏览/检索结果: 共8条，第1-8条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 Transient responses of deep-buried unlined tunnels subjected to blasting P wave 期刊论文  OAI收割 COMPUTERS AND GEOTECHNICS, 2022, 卷号: 146, 期号: -, 页码: - 作者:  Mei, Wanquan;  Xia, Yuanyou;  Pan, Peng-Zhi;  Li, Mei;  Tan, Sirong   |  收藏  |  浏览/下载：16/0  |  提交时间：2023/08/02 Rock mass damage  Transient disturbance  Dynamic responses  CASRock   Active Disturbance Rejection Control for a Fluid-Driven Hand Rehabilitation Device 期刊论文  OAI收割 IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2021, 卷号: 26, 期号: 2, 页码: 841-853 作者:  Li, Houcheng;  Cheng, Long;  Li, Zhengwei;  Xue, Wenchao   |  收藏  |  浏览/下载：27/0  |  提交时间：2021/06/07 Actuators  Exoskeletons  Performance evaluation  Training  IEEE transactions  Mechatronics  Active disturbance rejection control  extended state observer  extension motion  hand rehabilitation  parameter selection  transient  steady-state performance   Active Disturbance Rejection Control for a Fluid-Driven Hand Rehabilitation Device 期刊论文  OAI收割 IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2021, 卷号: 26, 期号: 2, 页码: 841-853 作者:  Li, Houcheng;  Cheng, Long;  Li, Zhengwei;  Xue, Wenchao   |  收藏  |  浏览/下载：26/0  |  提交时间：2021/10/26 Actuators  Exoskeletons  Performance evaluation  Training  IEEE transactions  Mechatronics  Active disturbance rejection control  extended state observer  extension motion  hand rehabilitation  parameter selection  transient  steady-state performance   Adaptive Neural Control of a Class of Stochastic Nonlinear Uncertain Systems With Guaranteed Transient Performance 期刊论文  OAI收割 IEEE TRANSACTIONS ON CYBERNETICS, 2020, 卷号: 50, 期号: 7, 页码: 2971-2981 作者:  Wang, Jianhui;  Liu, Zhi;  Zhang, Yun;  Chen, C. L. Philip;  Lai, Guanyu   |  收藏  |  浏览/下载：23/0  |  提交时间：2020/08/03 Neural networks  Adaptive systems  Nonlinear systems  Backstepping  Transient analysis  Approximation error  Time-varying systems  Adaptive control  neutral network  nonlinear control  stochastic disturbance  transient performance   Performance analysis of active disturbance rejection tracking control for a class of uncertain LTI systems 期刊论文  OAI收割 ISA TRANSACTIONS, 2015, 卷号: 58, 页码: 133-154 作者:  Xue, Wenchao;  Huang, Yi   |  收藏  |  浏览/下载：18/0  |  提交时间：2018/07/30 Extended state observer (ESO)  Active disturbance rejection control (ADRC)  Tracking  Transient performance  Uncertain systems   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：28/0  |  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%   Control method research on wide flight envelope aerocraft (EI CONFERENCE) 会议论文  OAI收割 2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China 作者:  Duan Z. 收藏  |  浏览/下载：28/0  |  提交时间：2013/03/25 The flying qualities of aerocraft was directly effected by the autopilot  for the wide flight envelope aerocraft  on the basic of analyzing the typical trajectory  the three loop autopilots of roll stability  pitch and yaw were designed  using single-mode Transient suppression method  the overload due to control surface transition deflection was avoided when control parameters changing  the verification was done by non-linear simulation. The result showed that: Under the action of the disturbance torque  the maximum roll was less than 5  the range of the aerocraft was from 13.5km to 22.4km  the max height was about 5100m  the max deviation of lateral was about 42m  the maximum elevator deflection was less than 6.5 the control law was applicable within the effective range. An autopilot design method of wide flight envelope aerocraft was provided. 2011 IEEE.   Multiple bipolar structure of normal magnetic field at the magnetopause 期刊论文  OAI收割 Planetary and Space Science, 2003, 卷号: 51, 期号: 6, 页码: 381-386 陈涛; 刘振兴; Zhang, X. X. 收藏  |  浏览/下载：22/0  |  提交时间：2014/04/30 magnetopause  transient disturbance  reconnection  multiple bipolar  structure  flux-transfer events  x-line reconnection  dayside  magnetopause  isee  observations  surface-waves  pulsations  magnetosphere  magnetosheath  excitation  simulation