机构

• 自动化研究所 [7]
• 长春光学精密机械与物... [2]
• 国家空间科学中心 [1]
• 数学与系统科学研究院 [1]

采集方式

• OAI收割 [11]

内容类型

• 期刊论文 [10]
• 会议论文 [1]

发表日期

• 2023 [2]
• 2021 [1]
• 2020 [1]
• 2019 [1]
• 2018 [1]
• 2012 [1]
• 更多

学科主题

• 空间技术 [1]

筛选

浏览/检索结果: 共11条，第1-10条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 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：9/0  |  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：19/0  |  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：19/0  |  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：16/0  |  提交时间：2021/03/11 Adaptive control  attitude control  input quantization  spacecraft  time-varying inertial parameter   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：26/0  |  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：36/0  |  提交时间：2019/01/11 attitude control and momentum management  extended state observer  nonlinear control  velocity-free spacecraft  uncertainty attenuation   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   Finite-Time Attitude Tracking Control for Spacecraft Using Terminal Sliding Mode and Chebyshev Neural Network 期刊论文  OAI收割 IEEE TRANSACTIONS ON SYSTEMS MAN AND CYBERNETICS PART B-CYBERNETICS, 2011, 卷号: 41, 期号: 4, 页码: 950-963 作者:  Zou, An-Min;  Kumar, Krishna Dev;  Hou, Zeng-Guang;  Liu, Xi 收藏  |  浏览/下载：35/0  |  提交时间：2015/08/12 Adaptive control  attitude tracking  Chebyshev neural network (NN) (CNN)  spacecraft  terminal sliding mode (TSM)   Quaternion-Based Adaptive Output Feedback Attitude Control of Spacecraft Using Chebyshev Neural Networks 期刊论文  OAI收割 IEEE TRANSACTIONS ON NEURAL NETWORKS, 2010, 卷号: 21, 期号: 9, 页码: 1457-1471 作者:  Zou, An-Min;  Kumar, Krishna Dev;  Hou, Zeng-Guang 收藏  |  浏览/下载：39/0  |  提交时间：2015/08/12 Adaptive control  Chebyshev neural network (CNN)  output feedback  quaternion  spacecraft attitude   A 3-axis simulator for spacecraft attitude control research (EI CONFERENCE) 会议论文  OAI收割 2010 IEEE International Conference on Information and Automation, ICIA 2010, June 20, 2010 - June 23, 2010, Harbin, Heilongjiang, China 作者:  Dai L. 收藏  |  浏览/下载：30/0  |  提交时间：2013/03/25 This article presents the details of a new 3-axis simulator for spacecraft attitude control research and simulation. The air bearing allows the test bed to rotate about three axes with tiny friction. The attitude determination system consists of three fibre optical gyros  an inclinometer and a magnetometer. The actuator of the system consists of three reaction flywheels and four control moment gyros (CMG). Mathematical models of the sensors and actuators are given to help algorithm design. An extended Kalman filter was designed to provide attitude information for controller. Mathematical simulation results prove the attitude determination system can achieve high precision. A coulomb friction model of reaction wheels is given with experimental results. A friction compensation algorithm was developed to raise the pointing accuracy of the control system. The article also describes the details of the hardware structure. A PD stabilizing controller is implemented to test the validation of the whole control system at last. 2010 IEEE.