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Chinese Academy of Sciences Institutional Repositories Grid
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CAS IR Grid
机构
数学与系统科学研究院 [5]
长春光学精密机械与物... [1]
自动化研究所 [1]
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OAI收割 [7]
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期刊论文 [6]
会议论文 [1]
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2021 [1]
2020 [1]
2018 [2]
2017 [1]
2012 [1]
2011 [1]
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Attitude synchronization and rigid formation of multiple rigid bodies over proximity networks
期刊论文
OAI收割
AUTOMATICA, 2021, 卷号: 125, 页码: 10
作者:
Deng, Juan
;
Wang, Lin
;
Liu, Zhixin
  |  
收藏
  |  
浏览/下载:27/0
  |  
提交时间:2021/06/01
Rigid body
Attitude synchronization
Rigid formation
Collision avoidance
An intrinsic approach to formation control of regular polyhedra for reduced attitudes
期刊论文
OAI收割
AUTOMATICA, 2020, 卷号: 111, 页码: 8
作者:
Zhang, Silun
;
He, Fenghua
;
Hong, Yiguang
;
Hu, Xiaoming
  |  
收藏
  |  
浏览/下载:11/0
  |  
提交时间:2020/05/24
Attitude control
Distributed control
Formation control
Nonlinear systems
Decentralized cooperative tracking subject to motion constraints
期刊论文
OAI收割
AUTOMATICA, 2018, 卷号: 96, 页码: 121-126
作者:
Wang, Lin
;
Markdahl, Johan
;
Liu, Zhixin
;
Hu, Xiaoming
  |  
收藏
  |  
浏览/下载:35/0
  |  
提交时间:2018/11/16
Decentralized tracking
Formation control
Rigidity
Motion constraints
Attitude control
Intrinsic tetrahedron formation of reduced attitude
期刊论文
OAI收割
AUTOMATICA, 2018, 卷号: 87, 页码: 375-382
作者:
Zhang, Silun
;
Song, Wenjun
;
He, Fenghua
;
Hong, Yiguang
;
Hu, Xiaoming
  |  
收藏
  |  
浏览/下载:23/0
  |  
提交时间:2018/07/30
Attitude control
Distributed control
Formation control
Nonlinear systems
Relative attitude formation control of multi-agent systems
期刊论文
OAI收割
INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2017, 卷号: 27, 期号: 18, 页码: 4457-4477
作者:
Song, W.
;
Tang, Y.
;
Hong, Y.
;
Hu, X.
  |  
收藏
  |  
浏览/下载:18/0
  |  
提交时间:2018/07/30
attitude control
multi-agent systems
attitude formation
joint connectivity
asymptotic stability
Attitude Coordination Control for a Group of Spacecraft Without Velocity Measurements
期刊论文
OAI收割
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2012, 卷号: 20, 期号: 5, 页码: 1160-1174
作者:
Zou, An-Min
;
Kumar, Krishna Dev
;
Hou, Zeng-Guang
收藏
  |  
浏览/下载:55/0
  |  
提交时间:2015/08/12
Adaptive control
attitude coordination
Chebyshev neural networks (CNNs)
spacecraft formation flying (SFF)
without velocity measurements
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.