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Identification of the time-varying modal parameters of a spacecraft with flexible appendages using a recursive predictor-based subspace identification algorithm
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 233, 页码: 2032-2050
作者:
Ni, Zhiyu
;
Liu, Jinguo
;
Wu, Zhigang
收藏
  |  
浏览/下载:119/0
  |  
提交时间:2019/12/02
Modal parameter identification
recursive subspace algorithm
spacecraft
time-varying system
flexible appendage
Fuzzy Disturbance Observer-Based Sliding Mode Control for Liquid-Filled Spacecraft With Flexible Structure Under Control Saturation
期刊论文
IEEE Access, 2019, 卷号: Vol.7, 页码: 149810-149819
作者:
Liqian Dou
;
Miaomiao Du
;
Xiuyun Zhang
;
Hui Du
;
Wenjing Liu
收藏
  |  
浏览/下载:13/0
  |  
提交时间:2019/11/21
Space vehicles
Uncertainty
Liquids
Fuzzy logic
Stability analysis
Sliding mode control
Disturbance observers
Spacecraft
flexible vibration
liquid fuel slosh
control saturation
fuzzy disturbance observer
terminal sliding mode control
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
Identification of the time-varying modal parameters of a spacecraft with flexible appendages using a recursive predictor-based subspace identification algorithm
期刊论文
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019, 卷号: 233, 期号: 6, 页码: 2032-2050
作者:
Ni ZY(倪智宇)
;
Liu JG(刘金国)
;
Wu ZG(吴志刚)
收藏
  |  
浏览/下载:10/0
  |  
提交时间:2018/06/17
Modal parameter identification
recursive subspace algorithm
spacecraft
time-varying system
flexible appendage
Multi-objective integrated robust H infinity control for attitude tracking of a flexible spacecraft
期刊论文
ACTA ASTRONAUTICA, 2018, 卷号: 151, 页码: 80-87
作者:
Wu, Shunan
;
Chu, Weimeng
;
Ma, Xue
;
Radice, Gianmarco
;
Wu, Zhigang
收藏
  |  
浏览/下载:7/0
  |  
提交时间:2019/12/02
Attitude control
Flexible spacecraft
Robust control
Output feedback
Multi-objective
Identification of the time-varying modal parameters of a spacecraft with flexible appendages using a recursive predictor-based subspace identification algorithm
期刊论文
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2018, 页码: 1-19
作者:
Ni ZY(倪智宇)
;
Wu ZG(吴志刚)
;
Liu JG(刘金国)
;
Wang C(王超)
;
Yi RW(衣瑞文)
收藏
  |  
浏览/下载:29/0
  |  
提交时间:2018/06/17
Modal parameter identification
recursive subspace algorithm
spacecraft
time-varying system
flexible appendage
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
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