吴宝林

吴宝林，男，1983年出生，现任哈尔滨工业大学航天学院卫星技术研究所教授、博士生导师。他的研究领域包括航天器编队相对动力学与控制、航天器姿态控制与协同等。在地球扁率摄动下的编队动力学与控制理论问题上，吴宝林系统性地进行了研究，并提出了多种高精度的姿态控制与姿态协同控制方法。

• 1999年-2003年，哈尔滨工业大学，航天学院，飞行器设计专业，获学士学位

• 2003年-2005年，哈尔滨工业大学，航天学院，卫星技术研究所，获硕士学位

• 2007年-2011年，新加坡南洋理工大学，电机与电子工程学院，获博士学位

• 2018年04月-至今，哈尔滨工业大学，(校青年拔尖)副教授，博士生导师

• 2014年01月-2018年04月，哈尔滨工业大学，(校青年拔尖)副教授，硕士生导师

• 2013年06月-2013年12月，新加坡南洋理工大学，博士后

• 2011年02月-2013年05月，ST Electronics (Satellite Systems) Pte Ltd, Singapore，姿态控制工程师

• 2020年01月-至今，哈尔滨工业大学，教授。^[1]

• 航天器编队相对动力学与控制

• 航天器姿态控制与姿态协同

• 航天器轨道控制与优化

• 作为技术骨干参与重大标志性项目“月球轨道编队超长波天文观测微卫星”，该项目将在国际上首次实现在月球轨道上形成近距离航天器编队，将于2018年5月发射。负责研究双星编队构型初始化与构型维持的控制算法设计、控制软件的编程与测试。

• 本人作为技术负责人负责战支部队/航天八院的xx型号卫星编队控制系统研制。该型号为我国第一个立项的用于干涉成像的航天器编队飞行任务型号，将于2018年发射。

学术成果

Wang, Danwei, B. Wu, and E. K. Poh.Satellite Formation Flying. Springer Singapore, 2017.

SCI期刊学术论文第一作者或通信作者

Baolin Wu, and Xibin Cao, Robust Attitude Tracking Control for Spacecraft with Quantized Torques,Vol. 54, No. 2, April, 2018, pp. 1020-1028

Baolin Wu, Danwei Wang, Eng Kee Poh and Guangyan Xu, “Nonlinear Optimization of Low-thrust Trajectory for Satellite Formation: Legendre Pseudospectral Approach”, Journal of Guidance, Control, and Dynamics, Vol. 32, No. 4, 2009, Pages 1371-1381.

B. L. Wu, D. W. Wang, and E. K. Poh, “Decentralized Robust Adaptive Control for Attitude Synchronization under DirectedCommunication Topology”, Journal of Guidance, Control, and Dynamics, Vol. 34, No. 4, 2011, Pages: 1276-1282.

B. L. Wu, D. W. Wang, and E. K. Poh, “High-Precision Attitude Tracking Control for Satellite with Repeating Ground Track Orbit viaIterative Learning Control”, Journal of Guidance, Control, and Dynamics, Vol. 38, No. 3, 2014, Pages: 528-534

B. L. Wu, “Spacecraft Attitude Control with Input Quantization”, Journal of Guidance, Control, and Dynamics, 2015

Jitang Guo, Baolin Wu, Yunhai Geng, Xianren Kong, and Zhili Hou, Rapid SGCMGs Singularity-Escape Steering Law in Gimbal Angle Space, IEEE Transactions on Aerospace and Electronic Systems, In Press

J Zhang, Z Zhang, B Wu,Decentralized adaptive sliding mode control for beam synchronization of tethered InSAR system, Acta Astronautica 127, 57-66, 2016.

B Wu, G Xu, X Cao,Relative Dynamics and Control for Satellite Formation: Accommodating J2 Perturbation, Journal of Aerospace Engineering, 2016.

X Cao, B Wu,Indirect adaptive control for attitude tracking of spacecraft with unknown reaction wheel friction, Aerospace Science and Technology 47, 493-500, 2015

B Wu, X Cao, L Xing,Robust adaptive control for attitude tracking of spacecraft with unknown dead-zone, Aerospace Science and Technology 45, 196-202 2015

B Wu, D Wang, EK Poh,Decentralized sliding-mode control for spacecraft attitude synchronization under actuator failures, Acta Astronautica 105 (1), 333-343, 2014

B Wu, D Wang, EK Poh,Decentralized sliding‐mode control for attitude synchronization in spacecraft formation, International Journal of Robust and Nonlinear Control 23 (11), 1183-1197, 2013.

BL Wu, DW Wang, EK Poh,Energy-optimal low-thrust satellite formation manoeuvre in presence of J2 perturbation, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of, 2011.

B Wu, X Cao, Z Li,Multi-objective output-feedback control for microsatellite attitude control: An LMI approach, Acta Astronautica 64 (11), 1021-1031, 2009

B Wu, X Cao,Decentralized Control for Spacecraft Formation in Elliptic Orbits,Aircraft Engineering and Aerospace Technology, In Press.

Kui Zeng, Yunhai Geng, Baolin Wu, Shape-Based Analytic Safe Trajectory Design for Spacecraft Equipped with Low-Thrust Engines, Aerospace Science and Technology, Vol. 62, March 2017, Pages 87–97.

Xibin Cao, Baolin Wu, Robust Spacecraft Attitude Tracking Control Using Hybrid Actuators with Uncertainties, Acta Astronautica, Vol. 136, 2017, pp. 1-8

Jitang Guo, Yunhai Geng, Baolin Wu*, and Xianren Kong, Vibration Suppression of Flexible Spacecraft during Attitude Maneuver Using CMGs, Aerospace Science and Technology, Volume 72, January 2018, Pages 183-19

Baolin Wu, Qiang Shen, and Xibin Cao, Event-Triggered Attitude Control of Spacecraft, Advances in Space Research, Vol. 61, Issue 3, 1 February 2018, Pages 927-934

Yabo Hu, Baolin Wu, Yunhai Geng and YunhuaWu, Smooth Time-Optimal Attitude Control of Spacecraft,Part G: Journal of Aerospace Engineering(2018): 0954410018776531^[2].

Kui Zeng, Baolin Wu, and Yunhai Geng, Two-Phase Shaping Approach to Low-Thrust Trajectories Design Between Coplanar Orbits, Advances in Space Research, , 2018.

Baolin Wu, Danwei Wang, and Eng Kee Poh. Cyclic Formation Control for Satellite Formation Using Local Relative Measurement, Control and Intelligent Systems, Vol. 40, No. 1, 2012, pp. 11-21.

李冬柏，吴宝林*,张迎春, 考虑未知飞轮摩擦力矩的航天器姿态跟踪鲁棒自适应控制，宇航学报 37(2), 2016, pp.175-181.

李冬柏, 解延浩, 吴宝林, 考虑执行器安装偏差的航天器姿态跟踪控制，宇航学报 38(6), 2017, pp. 598-604.

吴宝林, 曹喜滨, 任子武, “一种长期稳定的卫星编队队形优化设计方法”, 航空学报, Vol. 28, No. 1, 2007, pp. 167-172.

吴宝林, 曹喜滨, 摄动椭圆参考轨道的相对运动状态转移方程, 宇航学报, Vol. 26, No. 6, 2005, pp. 702-706.

吴宝林, 曹喜滨, 基于模型预测的卫星编队队形机动控制, 吉林工业大学学报工学版，2007年第一期, pp. 218-223

Zhou Hao, Wang Danwei, and Wu Baolin, Time-Optimal Reorientation for Rigid Satellite with Reaction Wheels, International Journal of Control. Vol. 85, No. 10, October 2012, pp. 1452–1463.

Xinbin Cao, Chengfei Yue, Ming Liu, and Baolin Wu, Time Efficient Spacecraft Maneuver Using Constrained Torque Distribution, Acta Astronautica, Vol. 123, 2016, pp. 320-329.

Rigid-body attitude stabilization with attitude and angular rate constraints, Automatica, 2018.

Qiang Shen, Chengfei Yue, Cher Hiang Goh, Baolin Wu, and Danwei Wang, Rigid-body attitude tracking control under actuator faults and angular velocity constraints,IEEE/ASME Transactions on Mechatronics, 2018, In Press

耿云海, 刘伟星, 吴宝林, 转动惯量未知的再入飞行器姿态容错控制，宇航学报, 已录用.

Baolin Wu, Xibin Cao, Satellite Formation Keeping Using Robust Constrained Model Predictive Control.

Baolin Wu; Xibin Cao, Fuchun Liu; Synthesis for Satellite Formation Keeping: an LMI Approach, 1st International Symposium on Systems and Control in Aerospace and Astronautics, 19-21, Jan. 2006.

Bao-Lin Wu; Dong-Lei He; Xi-Bin Cao; Multi-Objective Output-Feedback Control for Satellite Formation Keeping: An LMI Approach, Machine Learning and Cybernetics, 2006 International Conference on, 13-16 Aug. 2006.

Baolin Wu, Danwei Wang, Guangyan Xu and Hang Yue, Nonlinear Optimization of Low-Thrust Trajectory for Satellite Formation: Legendre Pseudospectral Approach, AAS/AIAA Space Flight Mechanics Meeting, Galveston, Texas, USA, 27-31 Jan. 2008.

Baolin Wu, Eng Kee Poh, Wang, Danwei; Xu, Guangyan, Satellite Formation Keeping via Real-Time Optimal Control and Iterative Learning Control.

Xu, Guangyan; Poh, Eng Kee; Wang, Danwei; Baolin Wu, In-Plane Satellite Formations in Eccentric Orbits under J2 Perturbation,.

Xu, Guangyan; Poh, Eng Kee; Wang, Danwei; Baolin Wu, Periodic and Quasi-Periodic Satellite Relative Orbits at Critical Inclination, IEEE Aerospace conference, Big Sky, MT, USA, 7-14 March 2009.

Baolin Wu, Eng Kee Poh, Wang, Danwei, Decentralized Control for Satellite Formation Using Local Relative Measurements Only

Baolin Wu, Eng Kee Poh, Wang, Danwei, Decentralized Attitude Coordinated Control without Velocity Measurements for Spacecraft Formation, the 8th IEEE International Conference on Control & Automation. Xiamen, China, June 9-11, 2010.

Baolin Wu, Danwei Wang, High-Precision Attitude Control for Satellite with Repeat Ground Track Orbit , Control & Automation (ICCA), 11th IEEE International Conference on, 1145-1149, 2014.

Kui Zeng, Yunhai Geng, Baolin Wu, Chengqing Xie, A Novel Shape-Based Approximation Method for Constrained Low-Thrust Trajectory Design, AIAA/AAS Astrodynamics Specialist Conference, 5637, 2016.

Dongbai Li, Xueqin Chen, and Baolin Wu, Analysis of Reaction-Wheels Imbalance Torque Effects on Satellite Attitude Control System, Control and Decision Conference (CCDC), 2016 Chinese, 3722-3725.

Qiang Shen, Cher Hiang Goh, Chengfei Yue, and Baolin Wu, Spacecraft Reorientation Control with Attitude and Velocity Constrains, Aerospace Conference, 2017 IEEE, 1-7

Qiang Shen, Chengfei Yue, CH Goh, Baolin Wu, and Danwei Wang, Angular Rate Constrained Attitude Reorientation of Rigid Body, Control & Automation (ICCA), 2017 13th IEEE International Conference on, 165-169.