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清华大学 [13]
北京航空航天大学 [3]
长春光学精密机械与物... [2]
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期刊论文 [17]
会议论文 [5]
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Robust nonlinear controller design for uncertain hypersonic vehicles
期刊论文
CEAS Aeronautical Journal, 2019, 卷号: 10, 页码: 357-366
作者:
Liu, H.
;
Zhang, J.
;
Xi, J.
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浏览/下载:13/0
  |  
提交时间:2019/12/30
Closed loop control systems
Feedback linearization
Hypersonic aerodynamics
Hypersonic vehicles
Linear control systems
Robust control
Feedback linearization controllers
Feedback linearization technique
Non linear control
Nonlinear controller designs
Nonlinear information
Parametric uncertainties
Robust controller design
Robust non-linear controls
Controllers
Tracking control of quad-rotor based on non-regular feedback linearization
期刊论文
Lecture Notes in Electrical Engineering, 2018, 卷号: 460, 页码: 363-371
作者:
Lixia, Y.
;
Baoli, M.
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浏览/下载:8/0
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提交时间:2019/12/30
Errors
Feedback
Intelligent systems
Linearization
Navigation
Tracking (position)
Feedback linearization technique
Input transformation
Position tracking errors
Quad rotors
Three dimensional space
Tracking control problem
Tracking controller
Tracking controls
Feedback linearization
A sliding-mode variable-structure controller based on exact feedback linearization for automatic navigation system
期刊论文
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)
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浏览/下载:71/0
  |  
提交时间:2016/11/17
agricultural machine
affine nonlinear kinematics model
exact feedback linearization
sliding-mode variable-structure controller
新型变速恒频风力发电系统的非线性控制器设计
期刊论文
太阳能学报, 2015, 卷号: 36, 期号: 10, 页码: 2429-2434
作者:
Li, Fuzhu[1]
;
Wen, Chen[2]
;
Wang, Cuntang[3]
;
Guo, Yuqin[4]
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  |  
浏览/下载:2/0
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提交时间:2019/12/24
液压无级调速系统 风力发电 变速恒频 非线性控制器 反馈线性化 hydraulic stepless speed regulation system wind power generation variable-speed-constant-frequency (VSCF) non-linear controller feedback linearization
Feedback Linearization Design for Permanent Magnet Synchronous Motor With Disturbance Observer
会议论文
2013 32ND CHINESE CONTROL CONFERENCE (CCC), 2013-01-01
作者:
Chai Haoyu
;
Yan Peng
;
Guo Lei
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浏览/下载:1/0
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提交时间:2020/01/06
Permanent Magnet Synchronous Motor
Speed Controller
Nonlinear Disturbance Observer
Feedback Linearization Control
Reentry guidance based on feedback linearization (EI CONFERENCE)
会议论文
2011 International Conference on Electronics, Communications and Control, ICECC 2011, September 9, 2011 - September 11, 2011, Ningbo, China
Li D.-W.
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浏览/下载:23/0
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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
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.
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浏览/下载:13/0
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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.
Fuzzy disturbance observer based attitude controller design for spacecraft
会议论文
作者:
Zhi, Qiang
;
Cai, Yuan-Li
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浏览/下载:5/0
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提交时间:2019/12/10
Attitude controller
Differential geometry theory
Feedback linearization methods
Feedback linearization technique
Fuzzy basis functions
Fuzzy disturbance observers
Orthogonal reaction
Reaction flywheels
Output tracking control of single-phase arc furnace electrode regulator system based on feedback linearization
期刊论文
2010, 2010
Liu Xiao-he
;
Liu Si-jia
;
Zhang Yao-hui
;
Guan Ping
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浏览/下载:6/0
Robust guidance law design based on active disturbance rejection control
期刊论文
2010, 2010
Zhang Chenguang
;
Chen Darong
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浏览/下载:7/0
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