中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
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CAS IR Grid
机构
自动化研究所 [7]
长春光学精密机械与物... [3]
紫金山天文台 [2]
国家空间科学中心 [1]
数学与系统科学研究院 [1]
西安光学精密机械研究... [1]
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OAI收割 [15]
内容类型
期刊论文 [13]
会议论文 [2]
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2023 [2]
2021 [1]
2020 [1]
2019 [2]
2018 [1]
2015 [1]
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学科主题
天文和天体物理 [1]
空间技术 [1]
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Sliding-Mode-Based Attitude Tracking Control of Spacecraft Under Reaction Wheel Uncertainties
期刊论文
OAI收割
IEEE/CAA Journal of Automatica Sinica, 2023, 卷号: 10, 期号: 6, 页码: 1475-1487
作者:
Wei Chen
;
Qinglei Hu
  |  
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2023/05/29
Actuator failures
actuator misalignment angles
finite time
sliding mode control (SMC)
spacecraft attitude tracking
Coupled Dynamics and Integrated Control for Position and Attitude Motions of Spacecraft: A Survey
期刊论文
OAI收割
IEEE/CAA Journal of Automatica Sinica, 2023, 卷号: 10, 期号: 12, 页码: 2187-2208
作者:
Feng Zhang
;
Guangren Duan
  |  
收藏
  |  
浏览/下载:16/0
  |  
提交时间:2023/10/31
Coupled position and attitude dynamic modeling
integrated position and attitude control
position and attitude coupling analysis
spacecraft
space missions
Iterative Learning Disturbance Observer Based Attitude Stabilization of Flexible Spacecraft Subject to Complex Disturbances and Measurement Noises
期刊论文
OAI收割
IEEE/CAA Journal of Automatica Sinica, 2021, 卷号: 8, 期号: 9, 页码: 1576-1587
作者:
Tongfu He
;
Zhong Wu
  |  
收藏
  |  
浏览/下载:17/0
  |  
提交时间:2021/09/03
Disturbance observer
iterative learning
measurement noise
spacecraft attitude control
Robust Adaptive Attitude Control for Non-rigid Spacecraft With Quantized Control Input
期刊论文
OAI收割
IEEE/CAA Journal of Automatica Sinica, 2020, 卷号: 7, 期号: 2, 页码: 472-481
作者:
Yun Li
;
Fan Yang
  |  
收藏
  |  
浏览/下载:15/0
  |  
提交时间:2021/03/11
Adaptive control
attitude control
input quantization
spacecraft
time-varying inertial parameter
Star Identification Algorithm Based on Oriented Singular Value Feature and Reliability Evaluation Method
期刊论文
OAI收割
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2019, 卷号: 62, 期号: 5, 页码: 265-274
作者:
Wei, Xin
;
Wen, Desheng
;
Song, Zongxi
;
Xi, Jiangbo
  |  
收藏
  |  
浏览/下载:84/0
  |  
提交时间:2019/09/23
Star Identification
Star Sensor
Spacecraft
Attitude Determination
Vector Control-Based Singularity Avoidance/Escape Steering Law for Single Gimbal Control Moment Gyros
期刊论文
OAI收割
Ieee Access, 2019, 卷号: 7, 页码: 175727-175743
作者:
N.Mao
;
T.Zhang
;
K.Xu
;
M.S.Chen
;
C.Dong
  |  
收藏
  |  
浏览/下载:24/0
  |  
提交时间:2020/08/24
Steering law,SGCMG,satellite attitude control,logic,spacecraft,sgcmg,Computer Science,Engineering,Telecommunications
An integrated solution to ACMM problem of spacecraft with inertia uncertainty
期刊论文
OAI收割
INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2018, 卷号: 28, 期号: 17, 页码: 5575-5589
作者:
Liu, Ping
;
Xue, Wenchao
;
Chen, Sen
;
Huang, Yi
;
Sun, Zhendong
  |  
收藏
  |  
浏览/下载:34/0
  |  
提交时间:2019/01/11
attitude control and momentum management
extended state observer
nonlinear control
velocity-free spacecraft
uncertainty attenuation
Attitude stability of a dual-spin spacecraft on a stationary orbit around an asteroid subjected to gravity gradient torque
期刊论文
OAI收割
ASTROPHYSICS AND SPACE SCIENCE, 2015, 卷号: 355, 期号: 2, 页码: 203-212
作者:
Zhang, Ming-Jiang
;
Zhao, Chang-Yin
收藏
  |  
浏览/下载:25/0
  |  
提交时间:2015/12/03
Attitude stability
Dual-spin spacecraft
Asteroid
Conditions of stability
Attitude stability of a spacecraft with two flexible solar arrays on a stationary orbit around an asteroid subjected to gravity gradient torque
期刊论文
OAI收割
ASTROPHYSICS AND SPACE SCIENCE, 2014, 卷号: 351, 期号: 2, 页码: 507-524
作者:
Zhang, Ming-Jiang
;
Zhao, Chang-Yin
收藏
  |  
浏览/下载:28/0
  |  
提交时间:2014/11/20
Spacecraft
Asteroid
Attitude stability
Sufficient conditions of stability
Stability domain
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