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Chinese Academy of Sciences Institutional Repositories Grid
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自动化研究所 [3]
长春光学精密机械与物... [2]
沈阳自动化研究所 [2]
数学与系统科学研究院 [1]
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OAI收割 [8]
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期刊论文 [4]
会议论文 [2]
学位论文 [2]
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2023 [1]
2020 [1]
2019 [1]
2017 [1]
2012 [1]
2011 [2]
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Constrained Moving Path Following Control for UAV With Robust Control Barrier Function
期刊论文
OAI收割
IEEE/CAA Journal of Automatica Sinica, 2023, 卷号: 10, 期号: 7, 页码: 1557-1570
作者:
Zewei Zheng
;
Jiazhe Li
;
Zhiyuan Guan
;
Zongyu Zuo
  |  
收藏
  |  
浏览/下载:10/0
  |  
提交时间:2023/06/14
Moving path following (MPF)
robust control barrier function
safety margin
shipboard landing
unmanned aerial vehicle (UAV)
Robust Control of an Aerial Manipulator Based on a Variable Inertia Parameters Model
期刊论文
OAI收割
IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2020, 卷号: 67, 期号: 11, 页码: 9515-9525
作者:
Zhang GY(张广玉)
;
He YQ(何玉庆)
;
Dai B(代波)
;
Gu F(谷丰)
;
Liu GJ(刘光军)
  |  
收藏
  |  
浏览/下载:35/0
  |  
提交时间:2020/08/08
Manipulator dynamics
Couplings
Vehicle dynamics
Unmanned aerial vehicles
Force
Robustness
Aerial manipulator
disturbance rejection
dynamic modeling
unmanned aerial vehicle (UAV) control
Robust Adaptive Tracking Control for Quadrotors by Combining PI and Self-Tuning Regulator
期刊论文
OAI收割
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2019, 卷号: 27, 期号: 6, 页码: 2663-2671
作者:
Lei, Wenchao
;
Li, Chanying
;
Chen, Michael Z. Q.
  |  
收藏
  |  
浏览/下载:42/0
  |  
提交时间:2020/05/24
Adaptation models
Adaptive control
Control systems
Dynamic scheduling
Robustness
Pulse width modulation
Proportional-integral (PI)
quadrotor
robust adaptive control
self-tuning regulator (STR)
tracking control
unmanned aerial vehicle (UAV)
Control techniques of tilt rotor unmanned aerial vehicle systems: A review
期刊论文
OAI收割
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 1, 页码: 135-148
作者:
Liu Z(刘重)
;
He YQ(何玉庆)
;
Yang LY(杨丽英)
;
Han JD(韩建达)
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2017/02/05
Aircraft structures
Dynamics modeling
Flight control
Tilt rotors
Unmanned aerial vehicle (UAV)
Trajectory tacking control of a quad-rotor based on active disturbance rejection control (EI CONFERENCE)
会议论文
OAI收割
2012 IEEE International Conference on Automation and Logistics, ICAL 2012, August 15, 2012 - August 17, 2012, Zhengzhou, China
Gong X.
;
Tian Y.
;
Bai Y.
;
Zhao C.
收藏
  |  
浏览/下载:29/0
  |  
提交时间:2013/03/25
The objective of this paper is to deal with a trajectory tracking of a Quad-rotor unmanned aerial vehicle (UAV). For the model uncertainty
the external disturbance and the coupling factor are considered
an active disturbance rejection control (ADRC) algorithm is introduced into the designing procedure. The aircraft dynamic model is proposed in this article
based on which the closed-loop control system is divided into four independent channels with the coupling factor compensated by the extended state observer (ESO). The nonlinear state error feedback (NLSEF) algorithm is designed in each channel to improve the closed-loop dynamics. In this article
the ADRC controller is expressed in the discrete form. And finally
the simulation results show that the proposed control algorithm achieves a favourable tracking performance. 2012 IEEE.
基于自抗扰控制的无人机抗风干扰自动起飞与着陆研究
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:
熊华
收藏
  |  
浏览/下载:335/0
  |  
提交时间:2015/09/02
无人机
起飞
着陆
风干扰
自抗扰控制
Unmanned Aerial Vehicle
UAV
takeoff
landing
wind disturbance
Active Disturbance Rejection Control
ADRC
Robust trajectory tracking control of autonomous quad-rotor UAV based on double loop frame (EI CONFERENCE)
会议论文
OAI收割
2011 International Conference on Materials, Mechatronics and Automation, ICMMA 2011, January 15, 2011 - January 16, 2011, Melbourne, VIC, Australia
作者:
Sun Q.
收藏
  |  
浏览/下载:22/0
  |  
提交时间:2013/03/25
This paper deals with the under-actuated characteristic of a quad-rotor unmanned aerial vehicle (UAV). By designing the double loop configuration
the autonomous trajectory tracking is realized. The model uncertainty
external disturbance and the senor noise are also taken into consideration. Then the H controller is put forward in the inner loop. An optimal stability augmentation control (SAC) method is used to stabilize the horizon position and keep it away from oscillation. By calculating the nonlinear decouple map
control quantity is converted to the speeds of the four rotors. At last some simulation results and the prototype implementation prove that the control method is effective.
多操纵面无人机控制分配技术研究
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, 2010
作者:
王会东
收藏
  |  
浏览/下载:180/0
  |  
提交时间:2015/09/02
无人机
控制分配
动态控制分配
实时控制分配
可重构飞行控制
UAV(Unmanned Aerial Vehicle)
Control allocation
Dynamic control allocation
Real-time control allocation
Reconfigurable flight control