人才培养

姜博严


  

姜博严

性别

出生年月

1987.06

民族

毕业学校

哈尔滨工业大学

毕业时间

2018.07

学位

博士

所学专业

控制科学与工程

行政职务

工作时间

2018.09

党派

中国民主同盟

职称

讲师

E-mail

jiangby@hhu.edu.cn

 

18861118929

社会

任职

很多期刊的审稿人

受教育

经历

2014.09—2018.07 哈尔滨工业大学航天学院控制科学与工程专业博士

工作

经历

201809河海大学常州校区物联网工程学院讲师

研究

方向

控制理论研究,包括非线性控制、有限时间控制、输出反馈控制、观测器设计、无人船控制、航天器控制等

论文

论著

 SCI检索期刊论文

(1) Boyan Jiang, Qinglei Hu, Michael I. Friswell*. Fixed-time   attitude control for rigid spacecraft with actuator saturation and faults[J].   IEEE Transactions on Control Systems   Technology, 2016, 24(5):1892-1898.(SCI收录号000381506100034, 影响因子IF=3.882)

(2) Boyan Jiang, Qinglei Hu,   Michael I. Friswell*. Fixed-time   rendezvous control of spacecraft with a tumbling target under loss of   actuator effectiveness[J]. IEEE Transactions   on Aerospace and Electronic Systems, 2016, 52(4):1576-1586. (SCI收录号000388648500017, 影响因子IF=1.975)

(3) Boyan Jiang, Chuanjiang Li* and Guangfu Ma. Finite-time output   feedback attitude control for spacecraft using “Adding a power integrator”   technique[J]. Aerospace Science and Technology,   2017, 66. (SCI收录号000403119700031, 影响因子IF=2.057)

(4) Qinglei Hu*(导师), Boyan Jiang. Observer-based output feedback attitude   stabilization for spacecraft with finite-time convergence[J]. IEEE Transactions on Control Systems   Technology, 2017 (网络已出版SCI检索, 影响因子IF=3.882)

(5) Qinglei Hu*(导师), Boyan Jiang. Continuous finite-time attitude control   for rigid spacecraft based on angular velocity observer[J]. IEEE Transactions on Aerospace and   Electronic Systems, 2017. (网络已出版SCI检索, 影响因子IF=1.975)

(6) Qinglei Hu*(导师), Boyan Jiang, Michael I. Friswell. Robust saturated   finite time output feedback attitude stabilization for rigid spacecraft[J]. Journal of Guidance Control and Dynamics,   2014, 37(6): 1914-1929,( SCI收录号000343924400013, 影响因子IF=1.856)

(7) Qinglei Hu*(导师), Boyan Jiang, Youmin Zhang. Output feedback attitude   tracking for spacecraft under control saturation and disturbance[J]. Journal of Dynamic Systems Measurement   and Control, 2016, 138(1): 011006.( SCI收录号000366319100006, 影响因子IF=1.388)

 EI检索期刊论文

(1) 姜博严, 胡庆雷*, 石忠. 与自由翻滚目标近距离段交会对接的相对姿轨耦合控制[J]. 宇航学报, 2014, 35(1):54-60. (EI检索, 影响因子IF: 1.232)

(2) 胡庆雷*(导师), 姜博严. 石忠. 基于新型终端滑模的航天器执行器故障容错姿态控制[J]. 航空学报, 2014, 35(1):249-258. (EI检索, 影响因子IF: 1.397)

 EI检索会议论文

(1) Boyan   Jiang, Chuanjiang Li*,   Yanning Guo, et al. Fixed-time Control Design for Spacecraft Attitude   Stablization. 27th AAS/AIAA Space Flight Mechanics Meeting, 2017, San   Antonio, USA, Feb. 5-9. (EI收录号:20174204271287)

(2) Boyan Jiang,   Chuanjiang Li*, Li Yuan, Guangfu. Finite-time output feedback control of   spacecraft attitude based on “adding a power integrator” method. Chinese   Control and Decision Conference (CCDC), 2017 29th Chinese. IEEE, Chongqing,   China, May 28-30, 2017, 6337-6342. (EI收录号20173504090352)

(3) Boyan   Jiang, Zhuo Chen, Qinglei Hu*,   Juntong Qi. Fixed-time attitude control for rigid spacecraft with external   disturbances[C]. Proceeding of the 11th World Congress on Intelligent Control   and Automation, WCICA 2015. (EI收录号20152600977323)

(4) Chuanjiang Li*, Boyan Jiang,   Qinghua Zhu, et al. Non-singular terminal sliding mode controller for   spacecraft attitude stabilization[C]. Chinese Control Conference (CCC), 2015   34th Chinese. IEEE,Hangzhou, China,    Jul. 28-30, 2015: 907-912. (EI收录号20154601538976)

(5) Zhong Shi, Boyan Jiang,   Qinglei Hu*, A Controller Design for Spacecraft with   Control Saturation Under Thrust Misalignment[C], Chinese Control and   Decision Conference (CCDC), 2013 25th Chinese. 2013, 2397-2402. (EI检索)

(6) Li Yuan, Boyan Jiang,   Chuanjiang Li*, et al. Fixed-time Control Design for Spacecraft Attitude   Stabilization. AAS/AIAA Astrodynamics Specialist Conference, ASC 2015, Vail,   USA, Aug. 10-13. (EI收录号:20165303202562)

2019年在审论文

(1)    Boyan   Jiang. Fixed-time Attitude   Tracking Control for Spacecraft based on Adding A Power Integrator Technique.   International Journal of Robust and Nonlinear Control

(2)    Boyan   Jiang. Time Estimation of Traditional Nonsingular   Terminal Sliding Mode Control for Double Integrator and Spacecraft Attitude   Stabilization. IEEE Transactions on   Control Systems Technology

(3)    Boyan   Jiang. Lyapunov-based   Finite-time Homogeneous Control for Perturbed Spacecraft Attitude   Stabilization. IEEE Transactions on   Control Systems Technology

(4) Boyan Jiang. Sub-fixed-time   control for a class of second order system. Transactions of the Institute   of Measurement and Control

(5) Boyan Jiang, Huanyu   Miao. Sub-fixed-time control of a class of nonlinear system with disturbance.   Chinese Control Conference

(6) Boyan Jiang, Yuqi   Su. Sub-fixed-time stability of a class of nonlinear system. Chinese Control   and Decision Conference

科研

成果

1.        国家自然科学基金青年项目,No. 61903123,航天器姿态稳定的有限时间控制方法研究,2020.01-2022.1226万,主持

2.        江苏省自然科学基金青年项目,No.BK20190165,有限时间控制方法研究及其在航天器姿态系统中的应用,2019.07-2022.0620万,主持

3.        江苏省2010-2020双创博士计划(世界名校类)

4.        河海大学中央高校基本科研业务费项目,No.2019B01114,二阶系统有限时间状态反馈控制问题研究,2019.01-2020.125万,主持

教学

工作

讲授本科课程:机电学院工业设计专业《电工技术基础》课程

物联网工程学院物联网专业《物联网控制》课程

讲授研究生课程:物联网工程学院检测技术与自动化装置研究生专业《自适应控制》课程

奖励

荣誉

江苏省“双创”人才;河海大学第四层次“大禹学者”支持