2013/9—2016/9 哈尔滨工业大学，控制科学与工程，博士研究生，导师：马广富，胡庆雷
2010/9—2013/4 中国民航大学，导航、制导与控制，硕士研究生，导师：石忠，高庆吉
2006/9—2010/7 河南大学，自动化，学士

2016/11—至今，上海海事大学，物流科学与工程研究院，智能港口物流协同创新中心，硕士生导师，讲师；
2013/05—2014/01，上海宇航系统工程研究所，飞行器控制与任务仿真研究室，实习工程师

1. 学术兼职：

[1] 中国自动化学会会员，导航、制导与控制专业委员会委员。

[2] Nonlinear Dynamics、ISA Transactions、Aerospace Science and Technology（2017年度优秀审稿人）、IET Control Theory & Applications、International Journal of Robust and Nonlinear Control 等多个学术期刊审稿人。

[3] The 2018 International Symposium on Sensing and Instrumentation in IoT Era，本地组委会委员，Session Chair。

2. 代表性论文 (近五年)

A 期刊论文

[1] Bo Li, Ke Qin, Bing Xiao and Yongsheng Yang, “Finite-time Extended State Observer based fault tolerant output feedback control for attitude stabilization,” ISA Transactions, Available online 8 February 2019, In Press. Doi: 10.1016/j.isatra.2019.01.039.  (SCI & EI)

[2] Bo Li, Qinglei Hu, Yongsheng Yang and Octavian A. Postolache, “Finite-time Disturbance Observer Based Integral Sliding Mode Control for Attitude Stabilization under Actuator Failure,” IET Control Theory & Applications, vol. 13, no. 1, pp. 50-58, January 2019. (SCI & EI)

[3] Bo Li, Qinglei Hu, Guangfu Ma and Yongsheng Yang, “Fault Tolerant Attitude Stabilization Incorporating Closed-loop Control Allocation,” IEEE Transactions on Aerospace and Electronic Systems, Published online, 2018, doi: 10.1109/TAES.2018.2880035. (SCI & EI)

[4] Bo Li, Qinglei Hu and Yongsheng Yang, “Continuous Finite-time Extended State Observer based Fault Tolerant Control for Attitude Stabilization,” Aerospace Science and Technology, vol. 89, pp. 204-213, January 2019. (SCI & EI)

[5] Bo Li, Qinglei Hu, Yanbo Yu and Guangfu Ma, “Observer-based Fault Tolerant Attitude Control for Rigid Spacecraft,” IEEE Transactions on Aerospace and Electronic Systems, vol. 53, no. 5, pp. 2572–2582, 2017. (SCI & EI,)

[6] Bo Li, Qinglei Hu and Guangfu Ma, “Extended State Observer based Robust Attitude Control of Spacecraft with Input Saturation,” Aerospace Science and Technology, 2016, 50: 173–182. (SCI & EI)

[7] Bo Li, Qinglei Hu and Juntong Qi, “Null-space-based Optimal Control Reallocation for Spacecraft Stabilization under Input Saturation,” International Journal of Adaptive Control and Signal Processing, 2015, 29(6): 705–724. (SCI & EI)

[8] Qinglei Hu, Bo Li, Danwei Wang and Eng Kee Poh, “Velocity-free Fault Tolerant Control Allocation for Flexible Spacecraft with Redundant Thrusters,” International Journal of Systems Science, 2015, 46(6): 976–922. (导师一作, SCI & EI)

[9] Qinglei Hu, Bo Li and Youmin Zhang, “Nonlinear Proportional-Derivative Control Incorporating Closed-loop Control Allocation for Spacecraft,” Journal of Guidance, Control, and Dynamics, 2014, 37(3): 799–812. (导师一作, SCI & EI)

[10] Qinglei Hu, Bo Li and Juntong Qi, “Disturbance Observer based Finite-time Attitude Control for Rigid Spacecraft under Input Saturation,” Aerospace Science and Technology, 2014, 39: 13–21. (导师一作, SCI & EI)

[11] 宋斌, 颜根廷, 李波, 郑鹏飞. 基于自抗扰技术的挠性航天器高精度指向控制. 上海航天, 2014, 31(2): 1–7.

B 会议论文

[1] Wen Liu, Jun Zhang, Bo Li, Yongsheng Yang and Octavian Adrian Postolache, Finite-time Formation Tracking Control for Quadrotor UAVs Based on Fast Non-singular Terminal Sliding Mode. The 1st International Symposium on Sensing and Instrumentation in IoT Era, Shanghai, China, September 6-7, 2018.(Best Paper Award, EI检索)

[2] Wenquan Gong, Jun Zhang, Bo Li and Yongsheng Yang, Integral-type Sliding Mode based Fault-tolerant Attitude Stabilization of A Quad-Rotor UAV. The 1st International Symposium on Sensing and Instrumentation in IoT Era, Shanghai, China, September 6-7, 2018.(EI检索)

[3] Hanyu Ban, Zhuoran Qi, Bo Li and Wenquan Gong, Nonlinear Disturbance Observer based Dynamic Surface Control for Trajectory Tracking of a Quadrotor UAV. The 1st International Symposium on Sensing and Instrumentation in IoT Era, Shanghai, China, September 6-7, 2018. (EI检索)

[4] Bo Li, Wen Liu, Wenquan Gong and Yongsheng Yang, Finite-time Disturbance Observer Based Attitude Stabilization Control under Actuator Failure. Proceeding of the 30th Chinese Control and Decision Conference, Shenyang, China, pp. 286-291, June 9-11, 2018. (EI检索)

[5] Guangfu Ma, Bo Li, Yanbo Yu and Qinglei Hu, Observer-based Fault Diagnosis Incorporating Adaptive Sliding Mode Control for Spacecraft Attitude Stabilization, Proceeding of the 34rd Chinese Control Conference, Hangzhou, China, pp. 6224–6229, July 28-30, 2015. (导师一作, EI检索)

[6] Bo Li, Qinglei Hu and Lei Guo, Observer based Inverse Optimal Attitude Stabilization Control of Spacecraft with Uncertainties, Proceeding of the 6th IEEE Chinese Guidance, Navigation and Control Conference, Yantai, China, pp. 269–274, August 8–10, 2014. (EI检索)