田栢苓
姓名 | 田栢苓 |
教师编号 | 19513 |
性别 | 男 |
学校 | 天津大学 |
部门 | 发明专利包写包过 加急申请 |
学位 | 发明专利包写包过 特惠申请 |
学历 | 版权登记666包过 代写全部资料 |
职称 | 副教授 |
联系方式 | 【发送到邮箱】 |
邮箱 | 【发送到邮箱】 |
人气 | |
软件产品登记测试 软件著作权666元代写全部资料 实用新型专利1875代写全部资料 集群智慧云企服 / 知识产权申请大平台 微信客服在线:543646 急速申请 包写包过 办事快、准、稳 |
田栢苓 教师名称:田栢苓 教师拼音名称:Tian Bailing 出生日期:1982-12-09 性别:男 学科:Control Theory and Control Engineering 职称:副教授 其他联系方式 邮箱:bailing_tian@tju.edu.cn 基本信息 研究方向 获奖情况 论文成果 Bailing Tian (M'11) received the B.S., M.S. and Ph.D degrees in automatic control from Tianjin University, Tianjin, China, in 2006, 2008 and 2011, respectively. He was an academic visitor at the School of Electrical and Electronic Engineering, University of Manchester from June 2014 to June 2015. He is currently an associate professor at the School of Electrical and Information Engineering, Tianjin University. His main research interests include finite time control and integrated guidance and control for hypersonic vehicles and multi-UAVs. Finite-Time Control and its Application in Hypersonic Vehicle and Multi-UAVs Integrated Guidance and Control for RLV 暂无内容 Wenru Fan, Bailing Tian*. Adaptive Multivariable Super-Twisting Sliding Mode Controller and Disturbance Observer Design for Hypersonic Vehicle, Mathematical Problems in Engineering, 2016. .2019 Qun Zong, Bailing Tian*, Liqian Dou and Chaofang Hu. Ascent Phase Trajectory Optimization for Vehicle with Space Restricted. Transactions of the Japan Society for Aeronautical and Space Sciences. 2011, 54(183):37-43. .2019 Linqi Ye, Qun Zong, Bailing Tian*, Fang Wang. Control-oriented Modeling and Adaptive Backstepping Control for a Nonminimum Phase Hypersonic Vehicle. ISA Transactions, 2017,70: 161-172. .2019 Shikai Shao, Qun Zong and Bailing Tian*. Finite-time output feedback attitude synchronization for multiple spacecraft, DOI: 10.1177/0142331217713075, 2017..2019 Shikai Shao, Qun Zong and Bailing Tian*. Finite-time sliding mode attitude control for rigid spacecraft without angular velocity measurement, Journal of the Franklin Institute, https://doi.org/10.1016/j.jfranklin.2017.04.020, 2017..2019 Ming You, Qun Zong, Bailing Tian*. Nonsingular terminal sliding mode control for reusable launch vehicle with atmospheric disturbances. Part G: Journal of Aerospace Engineering, DOI: 10.1177/0954410017708211, 2017..2019 Ming You, Qun Zong, Bailing Tian*, Zeng Fanlin. Fixed-time reentry attitude control based on nonsingular terminal sliding mode. IMA Journal of Mathematical Control and Information, 10.1093/imamci/dnx010,2017. .2019 Qi Dong, Qun Zong, Bailing Tian*. Adaptive disturbance observer based finite-time continuous fault tolerant control for reentry RLV. International Journal of Robust and Nonlinear Control, DOI:10.1002/rnc.3796, 2017. .2019 Qi Dong, Qun Zong, Bailing Tian* and Fang Wang. Integrated Finite-Time Disturbance Observer and Controller Design for Reusable Launch Vehicle in Reentry Phase, Journal of Aerospace Engineering, 2017,30(1):1-11..2019 Zongyu Zuo, Bailing Tian*, Michael Defoort, Zhengtao Ding. Fixed-time Consensus Tracking for Multi-agent Systems with High-order Integrator Dynamics, IEEE Transaction on Automatic Control, 10.1109/TAC.2017.2729502, 2017..2019 Linqi Ye, Qun Zong, Bailing Tian*, J.L.Crassidis. Output RedefinitionBased Dynamic Inversion Control for a Nonminimum Phase Hypersonic Vehicle. IEEE Transactions on Industrial Electronics, to appear, 2017, 10.1109/TIE.2017.2760246..2019 Bailing Tian and Qun Zong. Optimal Guidance for Reentry Vehicles Based on Indirect Legendre Pseudospectral Method. Acta Astronautica. 2011, 68(7-8):1176-1184. .2019 Bailing Tian, Wenru Fan, Qun Zong, Jie Wang and Fang Wang. Adaptive High Order Sliding Mode Controller Design for Hypersonic Vehicle with Flexible Body Dynamics. Mathematical Problems in Engineering, 2013..2019 Bailing Tian, Qun Zong, Jie Wang and Fang Wang. Quasi-continuous High-order Sliding Mode Controller Design for Reusable Launch Vehicles in Reentry Phase, Aerospace Science and Technology,28(1):198-207,2013..2019 Bailing Tian, Wenru Fan, Qun Zong, Jie Wang and Fang Wang. Nonlinear Robust Control for Reusable Launch Vehicles in Reentry Phase Based on Time-Varying High Order Sliding Mode. Journal of the Franklin Institute, 380(7):1787-1807, 2013..2019 Bailing Tian, Su Rui and Fan Wenru. Multiple Time Scale Smooth Second Order Sliding Mode Controller Design for Flexible Hypersonic Vehicles. Proceedings of The Institution of Mechanical Engineers Part G-journal of Aerospace Engineering, 229(5):781-791,2015..2019 Bailing Tian, Yan Xiaomo, Wang Hong. Fault-Tolerant Control Scheme For Manipulator with Actuator and Sensor Failure. International Journal of Advanced Mechatronic Systems, 64(6):166-173,2015..2019 Bailing Tian,Wenru Fan,Rui Su and Qun Zong. Nonlinear Robust Adaptive Deterministic Control for Flexible Hypersonic Vehicles in the Presence of Input Constraint, Asian Journal of Control, 17(6): 2303–2316,2015. .2019 Bailing Tian, Fan Wenru and Qun Zong. Integrated Guidance and Control for Reusable Launch Vehicle in Reentry Phase. Nonlinear Dynamics, 80(1-2):397-412,2015..2019 Bailing Tian, Fan Wenru and Qun Zong. Real-Time Trajectory and Attitude Coordination Control for Reusable Launch Vehicle in Reentry Phase. IEEE Transactions on Industrial Electronics, 62(3):1639-1650,2015..2019 Bailing Tian, Yin Liping and Wang Hong. Finite Time Reentry Attitude Control Based on Adaptive Multivariable Disturbance Compensation. IEEE Transactions on Industrial Electronics, 62(9): 5889-5898, 2015..2019 Bailing Tian, Zongyu Zuo and Hong Wang. Leader-Follower Fixed-Time Consensus of Multi-agent Systems with High-Order Integrator Dynamics, International Journal of Control, 90(7): 1420-1427, 2017. .2019 Bailing Tian, Zongyu Zuo, Xiaomo Yan and Hong Wang. A Fixed-time Output Feedback Control Scheme for Double Integrator Systems, Automatica, 80:17–24, 2017..2019 Bailing Tian, Hanchen Lu, Zongyu Zuo and Qun Zong. Multi-Variable Finite-Time Output Feedback Trajectory Tracking Control of Quadrotor Helicopters. International Journal of Robust and Nonlinear Control, 28:281-295,2018. .2019 Bailing Tian, Lihong Liu, Hanchen Lu and Zongyu Zuo. Multivariable Finite Time Attitude Control for Quadrotor UAV: Theory and Experimentation. IEEE Transactions on Industrial Electronics, 65(3): 2567-2577, 2018..2018 教育经历 2008.9-2011.6 Tianjin University Control Theory and Control Engineering 博士 2006.9-2008.6 Tianjin University Control Theory and Control Engineering 硕士 2002.9-2006.6 Tianjin University Automation 学士 工作经历 2015.7 -2019.12 |Tianjin University|Associate Professor 2014.6 -2015.6 |Manchester University|Visitor Scholar 2011.7 -2014.6 |Tianjin University|Lecturer |