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• 长春光学精密机械与物... [5]
• 力学研究所 [3]
• 金属研究所 [1]
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• OAI收割 [16]

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• 期刊论文 [10]
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• 2022 [2]
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• 空间技术 [1]

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浏览/检索结果: 共16条，第1-10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 Study of chattering suppression for the sliding mode controller of an electromagnetic levitation system 期刊论文  OAI收割 JOURNAL OF VIBRATION AND CONTROL, 2022, 页码: 13 作者:  Zhang, Weiwei;  Wu, Han;  Zeng, Xiaohui;  Liu, Mengjuan;  Ceng XH(曾晓辉)   |  收藏  |  浏览/下载：56/0  |  提交时间：2023/01/12 maglev vehicle  sliding mode control  rapid control prototyping  hardware experiments  non-linear control law   Research on Active Disturbance Rejection Control of Voice Coil Motor Based on Improved Particle Swarm Optimization 会议论文  OAI收割 ELECTR NETWORK, 2022-11-24 作者:  Wang, ZiYuan;  Ge, Wei   |  收藏  |  浏览/下载：9/0  |  提交时间：2023/06/19 Particle swarm optimization  space telescope  voice coil motor  active disturbance rejection control  non-linear expansion status observation   Adaptive neural network-based fault estimation for nonlinear systems with actuator faults in simultaneous multiplicative and additive forms 期刊论文  OAI收割 TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL, 2021, 页码: 12 作者:  Zhao, Yan;  Song, Minhang;  Huang, Xiangguo;  Chen, Ming   |  收藏  |  浏览/下载：30/0  |  提交时间：2022/06/15 Non-linear systems  fault tolerant control  actuator faults  RBF NN   Adaptive Nonlinear Hierarchical Control for a Rotorcraft Transporting a Cable-Suspended Payload 期刊论文  OAI收割 IEEE TRANSACTIONS ON SYSTEMS MAN CYBERNETICS-SYSTEMS, 2021, 卷号: 51, 期号: 7, 页码: 4171-4182 作者:  Liang X(梁潇);  Fang YC(方勇纯);  Sun N(孙宁);  Lin H(林河);  Zhao XG(赵新刚)   |  收藏  |  浏览/下载：40/0  |  提交时间：2021/07/06 Hierarchical control  Lyapunov methods  non linear control  rotorcraft transportation systems   A Linear Quadratic Controller Design Incorporating a Parametric Sensitivity Constraint 期刊论文  OAI收割 International Journal of Automation and Computing, 2019, 卷号: 16, 期号: 4, 页码: 553-562 作者:  Mohamed Yagoubi   |  收藏  |  浏览/下载：12/0  |  提交时间：2021/02/22 Linear quadratic control  parametric uncertainties  trajectory sensitivity  non-standard Riccati equation  Lur'e matrix equations  linear time invariant (LMI)  particle swarm optimization.   Dynamical modelling and control of space tethers: a review of space tether research 期刊论文  OAI收割 NONLINEAR DYNAMICS, 2014, 卷号: 77, 期号: 4, 页码: 1077-1099 作者:  Chen, Yi;  Huang, Rui;  He, Liping;  Ren, Xianlin;  Zheng, Bin   |  收藏  |  浏览/下载：18/0  |  提交时间：2018/03/15 Dynamics  Control  Non-linear  Space tether  Tethered system   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：27/0  |  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：25/0  |  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.   Control strategies and error compensation methods of high precision gyro stabilized platform (EI CONFERENCE) 会议论文  OAI收割 30th Chinese Control Conference, CCC 2011, July 22, 2011 - July 24, 2011, Yantai, China Deng K.; Cong S.; Shen H. 收藏  |  浏览/下载：22/0  |  提交时间：2013/03/25 Based on the principle of gyroscope and the structure of gyro stabilized platform  this paper gives the analysis and comparison of control strategies for stable platform included classical PID control  and three kinds of advanced strategies: Fuzzy Control  Sliding Mode Variable Structure Control and Active Disturbance Rejection Control. The compensation methods for stable platform's error are also discussed and evaluated based on the sources of error  especially for the non-linear friction and gyro drift. The paper provides the reliable methods for recognizing and improving the accuracy of gyro stabilized platform from the control strategies and error compensations. 2011 Chinese Assoc of Automation.   Nonlinear control design for system with mechanical resonance based on two tracking-differentiators (EI CONFERENCE) 会议论文  OAI收割 2010 IEEE International Conference on Mechatronics and Automation, ICMA 2010, August 4, 2010 - August 7, 2010, Xi'an, China 作者:  Li J.;  Li Y.;  Li Y.;  Li Y.;  Li Y. 收藏  |  浏览/下载：19/0  |  提交时间：2013/03/25 A nonlinear control strategy for controlling a motion system with mechanical resonance is presented in this paper. A mathematical model of the servo system is derived according to the parameters of an actual system. By using two Tracking-Differentiators  reference input and system output are tracked and their differential signals are given simultaneously. A nonlinear PD control law in velocity loop is designed based on non-smooth feedback. The simulation results show that the control law is superior remarkably in performance to linear PD control law and the classical PID control law. Tracking-Differentiator resolves the contradiction between rapidity and overshoot of system response. The nonlinear PD control law improves system dynamic performance and intensifies the ability of disturbance rejection. The control design achieved in this paper makes the servo system more robust. 2010 IEEE.