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科研机构
北京航空航天大学 [25]
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期刊论文 [19]
会议论文 [6]
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2019 [4]
2018 [5]
2017 [5]
2016 [2]
2015 [3]
2014 [2]
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专题:北京航空航天大学
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Gain-Scheduling Attitude Control for Complex Spacecraft Based on HOSVD
期刊论文
JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME, 2019, 卷号: 141
作者:
Lei, Bingyao
;
Shi, Peng
;
Wen, Changxuan
;
Zhao, Yushan
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2019/12/30
Attitude control
Control system synthesis
Flexible spacecraft
Scheduling
Singular value decomposition
Control implementation
Conventional controllers
Effectiveness and efficiencies
Higher order singular value decomposition
Linear parameter varying models
Robust gain-scheduling
Scheduling parameters
Weighting coefficient
Controllers
Extended harmonic disturbance observer-based attitude control for flexible spacecraft with control moment gyroscopes
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 233, 页码: 5331-5346
作者:
Huang, Liya
;
Wu, Zhong
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Flexible spacecraft
control moment gyroscopes
rotor imbalance
extended disturbance observer
harmonic disturbance observer
composite controller
Research on whole-spacecraft vibration isolation based on parallel load-bearing and damping system [并联式承载减振一体的整星隔振研究]
期刊论文
Lixue Xuebao/Chinese Journal of Theoretical and Applied Mechanics, 2019, 卷号: 51, 页码: 364-370
作者:
Pan, Z.
;
Xing, J.
;
Wang, L.
;
Chen, S.
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2019/12/30
Damping
Degrees of freedom (mechanics)
Fasteners
Flexible spacecraft
Launch vehicles
Natural frequencies
Rockets
Satellites
Ultrasonic devices
Damping characteristics
Multi degree of freedom systems
Parallel mode
Strength and stiffness
Transmission characteristics
Vibration attenuation
Viscous dampers
Whole spacecraft vibration isolations
Vibration analysis
A composite disturbance observer and H-infinity control scheme for flexible spacecraft with measurement delay and input delay
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 页码: 1472-1480
作者:
Qiao, Jianzhong
;
Li, Xiaofeng
;
Xu, Jianwei
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Disturbance observer (DO)
Flexible spacecraft
H-infinity control
Input delay
Measurement delay
Disturbance observer based attitude control for flexible spacecraft with input magnitude and rate constraints
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 72, 页码: 486-492
作者:
Liu, Zhijie
;
Liu, Jinkun
;
Wang, Lijun
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Flexible spacecraft
Input magnitude and rate constraints
Disturbance observer
State feedback control
LMI technology
Active Vibration Control of Flexible Satellites Using Solid Propellant Microthruster Array
期刊论文
JOURNAL OF AEROSPACE ENGINEERING, 2018, 卷号: 31
作者:
Yang, Bo
;
Fan, Zichen
;
Miao, Jun
;
Long, Jun
;
Liu, Xuhui
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Actuators
Asymptotic stability
Digital control systems
Discrete time control systems
Equations of state
Flexible structures
Piezoelectric actuators
Propellants
Riccati equations
Solid propellants
Spacecraft propulsion
Uncertainty analysis
Active vibration controls
Flexible satellites
Global asymptotic stability
Low-frequency vibration
Monte Carlo approach
Saturation problems
State-dependent Riccati equation
Switching strategies
Controllers
Dynamics of flexible multibody systems with variable-speed control moment gyroscopes
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 79, 页码: 554-569
作者:
Feng, Xiao
;
Jia, Yinghong
;
Xu, Shijie
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
Flexible multibody dynamics
Variable-speed control moment gyroscopes
Global matrix formulation
Spacecraft dynamics
Research on Microvibrations Generated by a Control Moment Gyroscope on a Flexible Interface Based on a Dynamic Substructure Method
期刊论文
INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2018, 卷号: 2018
作者:
Li, Xiongfei
;
Cheng, Wei
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
Computational efficiency
Degrees of freedom (mechanics)
Dynamic response
Flexible spacecraft
Frequency response
MATLAB
Connection interface
Control moment gyroscope
Degrees of freedom (DoFs)
Dynamic substructure
Frequency response functions
Multibody dynamics simulations
Prediction accuracy
Spacecraft structures
Gyroscopes
Robust fuzzy fault tolerant control for a class of nonlinear coupled ODE-beam systems
会议论文
2017 IEEE 56th Annual Conference on Decision and Control, CDC 2017
作者:
Feng, S.
;
Wu, H.-N.
收藏
  |  
浏览/下载:8/0
  |  
提交时间:2019/12/30
Fault tolerance
Flexible spacecraft
Ordinary differential equations
Bilinear matrix inequality
Coupled systems
Fault tolerant control
Lyapunov's direct method
Mild solution
Nonlinear beam equation
Nonlinear ordinary differential equation
Simulation studies
Nonlinear equations
Composite anti-disturbance attitude and vibration control for flexible spacecraft
期刊论文
IET CONTROL THEORY AND APPLICATIONS, 2017, 卷号: 11, 页码: 2383-2390
作者:
Sun, Haibin
;
Hou, Linlin
;
Zong, Guangdeng
;
Guo, Lei
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
space vehicles
vibration control
attitude control
variable structure systems
observers
estimation theory
aerospace control
control nonlinearities
composite anti-disturbance attitude control
vibration control
flexible spacecraft
attitude manoeuvre
attitude manoeuvre reduction
vibration reduction
external disturbances
finite-time integral sliding manifold
finite-time integral sliding mode disturbance observer
system states
flexible modal
lumped disturbance estimation va
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