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Chinese Academy of Sciences Institutional Repositories Grid
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CAS IR Grid
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长春光学精密机械与物... [5]
自动化研究所 [3]
沈阳自动化研究所 [1]
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OAI收割 [9]
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期刊论文 [5]
会议论文 [4]
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2020 [1]
2019 [2]
2018 [1]
2016 [1]
2013 [1]
2011 [2]
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Asymptotically stable critic designs for approximate optimal stabilization of nonlinear systems subject to mismatched external disturbances
期刊论文
OAI收割
NEUROCOMPUTING, 2020, 卷号: 396, 页码: 201-208
作者:
Zhao, Bo
;
Shi, Guang
;
Wang, Ding
  |  
收藏
  |  
浏览/下载:25/0
  |  
提交时间:2020/07/06
Adaptive dynamic programming
Adaptive critic designs
Mismatched external disturbances
Disturbance observer
Optimal control
Neural networks
Nested tuning law
Coordinated Formation Design of Multi-Robot Systems via an Adaptive-Gain Super-Twisting Sliding Mode Method
期刊论文
OAI收割
APPLIED SCIENCES-BASEL, 2019, 卷号: 9, 期号: 20, 页码: 19
作者:
Qian, Dianwei
;
Zhang, Guigang
;
Chen, Jiarong
;
Wang, Jian
;
Wu, Zhimin
  |  
收藏
  |  
浏览/下载:46/0
  |  
提交时间:2020/03/30
second order sliding mode control
adaptive control
formation control
multiple robots
super twisting law
Augmented fixed-time observer-based continuous robust control for hypersonic vehicles with measurement noises
期刊论文
OAI收割
IET CONTROL THEORY AND APPLICATIONS, 2019, 卷号: 13, 期号: 3, 页码: 422-433
作者:
Sun, Jinlin
;
Yi, Jianqiang
;
Pu, Zhiqiang
  |  
收藏
  |  
浏览/下载:72/0
  |  
提交时间:2019/07/12
linearisation techniques
observers
control system synthesis
vehicle dynamics
adaptive control
aircraft control
uncertain systems
robust control
variable structure systems
space vehicles
augmented fixed-time observer
measurement noises
cruise control
flexible air-breathing hypersonic vehicles
controller gains
finite-time convergence
fixed convergence time
FAHV
gain adaptation law
continuous robust control
input-output linearisation technique
Speed control for K-mirror of 2-m telescope using improved active disturbance rejection controller
期刊论文
OAI收割
Measurement, 2018, 卷号: 129, 页码: 245-255
作者:
Deng, Y. T.
;
Xia, P. P.
;
Li, H. W.
;
Wang, X. J.
  |  
收藏
  |  
浏览/下载:27/0
  |  
提交时间:2019/09/17
Turntable of K-mirror
Speed control
Active disturbance rejection
controller
Adaptive control law
unstable processes
network
Engineering
Instruments & Instrumentation
Adaptive controller design for underwater snake robot with unmatched uncertainties
期刊论文
OAI收割
SCIENCE CHINA-INFORMATION SCIENCES, 2016, 卷号: 59, 期号: 5, 页码: 1-15
作者:
Zhang AF(张安翻)
收藏
  |  
浏览/下载:64/0
  |  
提交时间:2016/06/21
underwater snake-like robot
adaptive control
simplified system
piecewise constant law
unmatched uncertainties
underactuated robots
High gain observer for drag tracking in mars entry longitudinal guidance (EI CONFERENCE)
会议论文
OAI收割
2012 International Conference on Measurement, Instrumentation and Automation, ICMIA 2012, September 15, 2012 - September 16, 2012, Guangzhou, China
Wu K.
;
Cui H.
;
Ma D.
;
Cui P.
收藏
  |  
浏览/下载:29/0
  |  
提交时间:2013/03/25
An extended high gain state and perturbation observer combined with feedback linearization was applied in drag tracking for Mars entry longitudinal guidance. The observer estimates the drag
the drag rate and the perturbation due to model uncertainty and disturbance for drag tracking. Mars entry simulation was performed to assess the performance of the adaptive guidance law. The results demonstrate that the proposed guidance law is robust to model error
and can recover the ideal performance of the feedback linearization control. Introduction In recent years
the concept of pinpoint landing has been proposed (2013) Trans Tech Publications
Switzerland.
Adaptive control at launching using three loop autopilot (EI CONFERENCE)
会议论文
OAI收割
2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China
作者:
Zhang Y.
收藏
  |  
浏览/下载:25/0
  |  
提交时间:2013/03/25
In order to guarantee the precise initial flight trajectory
control the missile disturbance of large disturbance torque
three loop adaptive autopilot was researched. The characteristics of the projectile and three loop autopilot instruction formation characteristics were analysed. From equivalent pitching angle of lateral acceleration feedback loop
combined with the instruction of generalized error
autopilot structure was simplified
and three loop autopilot adaptive control law and stability were designed. The test data show that when disturbance torque was 600Nm
the attitude angle generalized error was -4.4. In the time lasted about 15s
late trajectory accuracy was within 1.0.Three loop autopilot adaptive control law was able to control the disturbance of initial trajectory and adapt to dynamic characteristics changes
control system stability. It was the initial trajectory accurate solution method of flight. 2011 IEEE.
The application of the discrete sliding mode control based on state observer in aerial camera (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:
Zhang X.
;
Zhang X.
;
Zhang X.
收藏
  |  
浏览/下载:17/0
  |  
提交时间:2013/03/25
A discrete sliding mode control scheme based on state observer is designed for DC torque motor. Aim on the problem of control chattering and steady-state chattering caused by discrete sliding mode control method
adaptive reaching law is proposed Non-chattering and stability are made an analysis. The aerial camera is chosen as an experimental platform and the discrete sliding mode controller with adaptive reaching law is applied to the drawtube system
the value of acceleration can be observed on line. The experiment results show the control scheme can effectively eliminate chattering and also make the drawtube system achieve better dynamical performance. 2011 IEEE.
Adaptive sliding mode control for airborne Opto-Electronic platform servo system (EI CONFERENCE)
会议论文
OAI收割
7th International Conference on Machine Learning and Cybernetics, ICMLC, July 12, 2008 - July 15, 2008, Kunming, China
Wang C.-X.
;
Liu J.-H.
;
Shen H.-H.
;
Dai M.
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2013/03/25
The novel presents an adaptive reaching law sliding mode controller to slove a class of uncertain systems.The Airborne Opto-Electronic Platform sliding model is employed to represent a class of complex uncertain system. The control is based on reaching law control. Discrete time implementation of the sliding mode control strategy is considered in the paper
since it is more appropriate for practical applications. It is shown that the robustness of the sliding mode control method is constrained by sampling time. Design of the adaptive reaching law based on a discrete expotential reaching law concept is given
which to design a new sliding mode controller based on Lyapunov stability theory. The global asymptotic stability is guaranteed. An example with simulation results is given to illustrate the effectiveness of the proposed method. 2008 IEEE.