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Chinese Academy of Sciences Institutional Repositories Grid
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自动化研究所 [5]
沈阳自动化研究所 [5]
长春光学精密机械与物... [3]
数学与系统科学研究院 [2]
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OAI收割 [15]
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会议论文 [8]
期刊论文 [4]
学位论文 [3]
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2017 [1]
2016 [2]
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2011 [3]
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Composite Control of Nonlinear Singularly Perturbed Systems via Approximate Feedback Linearization
期刊论文
OAI收割
International Journal of Automation and Computing, 2020, 卷号: 17, 期号: 4, 页码: 610-620
作者:
Aleksey Kabanov
;
Vasiliy Alchakov
  |  
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2021/02/22
Approximate feedback linearization (AFL)
composite control
nonlinear singularly perturbed system
order reduction
decomposition.
A Composite Controller for Piezoelectric Actuators with Model Predictive Control and Hysteresis Compensation
会议论文
OAI收割
Nanjing, China, 2017-09-22
作者:
Wang, Ang
;
Cheng, Long
  |  
收藏
  |  
浏览/下载:14/0
  |  
提交时间:2018/05/04
Feedforward-feedback Control
Hysteresis Compensation
Model Predictive Control (Mpc)
Instantaneous Linearization
Piezoelectric Actuators (Peas)
Comparison of estimation and control methods for flexible needle in 2D
会议论文
OAI收割
28th Chinese Control and Decision Conference, CCDC 2016, Yinchuan, China, May 28-30, 2016
作者:
Zhao XG(赵新刚)
;
Guo, Hui
;
Ye D(叶丹)
;
Huo BY(霍本岩)
收藏
  |  
浏览/下载:31/0
  |  
提交时间:2016/09/13
Flexible Needle
Feedback Linearization
AKF
UKF
AUKF
A sliding-mode variable-structure controller based on exact feedback linearization for automatic navigation system
期刊论文
OAI收割
INTERNATIONAL JOURNAL OF AGRICULTURAL AND BIOLOGICAL ENGINEERING, 2016, 卷号: 9, 期号: 5, 页码: 158-165
作者:
Bai XP(白晓平)
;
Hu JT(胡静涛)
;
Gao L(高雷)
;
Zhang T(张天)
收藏
  |  
浏览/下载:87/0
  |  
提交时间:2016/11/17
agricultural machine
affine nonlinear kinematics model
exact feedback linearization
sliding-mode variable-structure controller
Flexible tip-steerable needle control with tissue uncertainty
会议论文
OAI收割
26th Chinese Control and Decision Conference, CCDC 2014, Changsha, China, May 31, 2014 - June 2, 2014
作者:
Zhao XG(赵新刚)
;
Kong, Lingguo
;
Ye D(叶丹)
;
Zhao YW(赵忆文)
;
Wu ZW(吴镇炜)
收藏
  |  
浏览/下载:26/0
  |  
提交时间:2014/11/03
Feedback linearization
Needles
State estimation
Uncertainty analysis
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:28/0
  |  
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.
无人机鲁棒非线性飞行控制技术研究
学位论文
OAI收割
工学博士, 中国科学院自动化研究所: 中国科学院研究生院, 2011
作者:
袁如意
收藏
  |  
浏览/下载:219/0
  |  
提交时间:2015/09/02
飞行控制
非线性控制
鲁棒控制
反馈线性化
反馈线性化
H∞控制
Backstepping算法
Flight Control
Flight Control
Robust Control
Feedback Linearization
Saturation Control
H∞Control
Backstepping
Reentry guidance based on feedback linearization (EI CONFERENCE)
会议论文
OAI收割
2011 International Conference on Electronics, Communications and Control, ICECC 2011, September 9, 2011 - September 11, 2011, Ningbo, China
Li D.-W.
收藏
  |  
浏览/下载:30/0
  |  
提交时间:2013/03/25
This paper presents a new reentry guidance algorithm for RLV (Reusable Launching Vehicle). The algorithm consists of two integrated components: trajectory planning algorithm and tracking algorithm. The most striking feature of algorithm here lies in that both planning and tracking are executed directly in height-velocity space
which is different from the methodology of configuration of drag in traditional shuttle guidance. In the session of trajectory planning
all trajectory constraints can be expressed with upper bound and lower bound in height-velocity space
then a linear interpolation is carried to search the nominal trajectory satisfying the requirement of downrange and target constraints. Then the tracking algorithm uses feedback linearization method to track this nominal profile and meet all constraints. Another typical feature of this algorithm is the strategy of downrange extension using FPA (flight path angle) controller to fulfill the requirement of large downrange. Proper combination of planning-tracking algorithm and FPA controller can bring great flexibility and adaptability to reentry guidance. The algorithm is proved to be robust enough to accommodate the model error and noises in the dynamics. 2011 IEEE.
Stability control of quad-rotor based on explicit model following with inverse model feedforward method (EI CONFERENCE)
会议论文
OAI收割
2011 IEEE International Conference on Mechatronics and Automation, ICMA 2011, August 7, 2011 - August 10, 2011, Beijing, China
Bai Y.
;
Gong X.
;
Hou Z.
;
Tian Y.
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2013/03/25
The quad-rotor is expected to carry out many different tasks. It is hoped that the quad-rotor can have different characteristics according to the different mission requirements. For this reason
a flight stability augmentation control system based on explicit model following with inverse model feedforward control method is proposed in this paper. This control system is composed of an explicit model
an inverse model and a feedback controller module. In order to calculate an inverse model of the coupled multivariable aircraft system
a feedback linearization loop is also applied to this control system. At last
simulations are performed to show the effectiveness of the designed stability augmentation control system in the presence of external disturbance and model uncertainty. The influence of explicit model to the characteristics of quad-rotor is also indicated in a contrast simulation result. 2011 IEEE.
Linearization of switched non-linear systems
期刊论文
OAI收割
TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL, 2010, 卷号: 32, 期号: 6, 页码: 677-705
作者:
Yuan, Yanyan
;
Qiao, Yupeng
;
Cheng, Daizhan
  |  
收藏
  |  
浏览/下载:18/0
  |  
提交时间:2018/07/30
Lie derivative
quotient vector field
semi-tensor product of matrices
singular state feedback
state feedback linearization
switched non-linear system