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浏览/检索结果: 共4条，第1-4条 帮助 已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择发表日期升序发表日期降序作者升序作者降序提交时间升序提交时间降序题名升序题名降序 Disturbance Observer Based Control for an Underwater Biomimetic Vehicle-Manipulator System with Mismatched Disturbances 会议论文 Suzhou, China, 2021.5.14-2021.5.16 作者:  Lv, Jiaqi;  Wang, Yu;  Wang, Shuo;  Cheng, Long;  Tan, Min 收藏  |  浏览/下载：4/0  |  提交时间：2023/06/25 Underwater biomimetic vehicle-manipulator system (UBVMS)  disturbance observer  arctangent non-singularity sliding mode controller (ANTSMC)  mismatched disturbances   Robust decentralized hybrid adaptive output feedback fuzzy control for a class of large-scale MIMO nonlinear systems and its application to AHS 期刊论文 ISA Transactions, 2014, 卷号: 53, 期号: 5, 页码: 1569-1581 作者:  Huang, Yi-Shao;  Liu, Wel-Ping*;  Wu, Min;  Wang, Zheng-Wu 收藏  |  浏览/下载：5/0  |  提交时间：2019/12/03 Large-scale systems  Nonlinear systems  MIMO systems  Combined adaptive fuzzy control  Output feedback  Decentralized control  Controller singularity   Robust decentralized adaptive fuzzy control for a class of large-scale MIMO nonlinear systems 期刊论文 International Journal of Robust and Nonlinear Control, 2012, 卷号: 22, 期号: 15, 页码: 1720-1742 作者:  Huang, Yi-Shao* 收藏  |  浏览/下载：3/0  |  提交时间：2019/12/03 large‐scale nonlinear systems  robust adaptive control  fuzzy control  decentralized control  controller singularity   United steering of control moment gyros for small satellite with limited gimbal rate (EI CONFERENCE) 会议论文 2010 IEEE International Conference on Information and Automation, ICIA 2010, June 20, 2010 - June 23, 2010, Harbin, Heilongjiang, China Xu K.; Jin G.; Chen C. 收藏  |  浏览/下载：17/0  |  提交时间：2013/03/25 Single Gimbal Control Moment Gyroscopes (SGCMG) can could provide large control torque and quick attitude maneuver rate to small satellites without any increase in power  volume and mass  which will help small satellites become more powerful. Singularity avoidance and failure steering are two important problems to SGCMGs and also the main focus in this field. A new united steering law for SGCMGs with capabilities of singularity avoidance and quick transition of singularity surfaces is developed in this paper. To ensuring the existence of null motion  the commanded output of controller was changed real-timely as the variation of singularity measurement of SGCMGs  which can avoid the gimbal angle rate saturation. This developed steering law could help the SGCMGs provide real-time control toques in spite of limitation of gimbal angle rate. Simulation analysis is conducted for a certain 4-SGCMG system mounted on a small satellite. Simulation results indicate that the steering law is very effective in singularity avoidance. 2010 IEEE.