姓 名 | 姜博严 | 性别 | 男 | 出生年月 | 1987.06 | 民族 | 汉 | |||
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 | 无 | 工作时间 | 2018.09 | 党派 | 中国民主同盟 | |||||
职称 | 讲师 | jiangby@hhu.edu.cn | 电 话 | 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 | 2018年09月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 | 一 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，待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，待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) 二 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) 三 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) 四2019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，2020.01-2022.12，26万，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，2019.07-2022.06，20万，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，2019.01-2020.12，5万，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 | |||||||||
