吳寶林[哈爾濱工業大學副教授]

吳寶林，男，博士後 ，(校青年拔尖)副教授 ，博士生導師 ，哈爾濱工業大學航天學院衛星技術研究所。

教育背景

•1999年-2003年，哈爾濱工業大學，航天學院，飛行器設計專業，獲學士學位 [1]

•2003年-2005年，哈爾濱工業大學，航天學院，衛星技術研究所，獲碩士學位 [1]

•2007年-2011年，新加坡南洋理工大學，電機與電子工程學院，獲博士學位 [1]

工作履歷

•2018年04月-至今，哈爾濱工業大學，(校青年拔尖)副教授，博士生導師

•2014年01月-2018年04月，哈爾濱工業大學，(校青年拔尖)副教授，碩士生導師 [1]

•2013年06月-2013年12月，新加坡南洋理工大學，博士後 [1]

•2011年02月-2013年05月，ST Electronics (Satellite Systems) Pte Ltd, Singapore，姿態控制工程師 [1]

研究領域

•太空飛行器編隊相對動力學與控制 [1]

•太空飛行器姿態控制與姿態協同

•太空飛行器軌道控制與最佳化

科研項目

•作為技術骨幹參與重大標誌性項目“月球軌道編隊超長波天文觀測微衛星”，該項目將在國際上首次實現在月球軌道上形成近距離太空飛行器編隊，將於2018年5月發射。負責研究雙星編隊構型初始化與構型維持的控制算法設計、控制軟體的編程與測試 [1]。

•本人作為技術負責人負責戰支部隊/航天八院的xx型號衛星編隊控制系統研製。該型號為我國第一個立項的用於干涉成像的太空飛行器編隊飛行任務型號，將於2018年發射 [1]。

學術成果

代表著作

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

SCI期刊學術論文(第一作者或通信作者)

[1] Baolin Wu, and Xibin Cao, Robust Attitude Tracking Control for Spacecraft with Quantized Torques, IEEE Transactions on Aerospace and Electronic Systems, Vol. 54, No. 2, April, 2018, pp. 1020-1028

[2] 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.

[3] 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.

[4] 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

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

[6] 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

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

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

[9]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

[10]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

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

[12]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.

[13]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.

[14]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

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

[16] 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.

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

[18] 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

[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

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

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

其它期刊論文

[1] 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.

[2] 李冬柏,吳寶林*,張迎春, 考慮未知飛輪摩擦力矩的太空飛行器姿態跟蹤魯棒自適應控制,宇航學報 37(2), 2016, pp.175-181.

[3] 李冬柏, 解延浩, 吳寶林, 考慮執行器安裝偏差的太空飛行器姿態跟蹤控制,宇航學報 38(6), 2017, pp. 598-604.

[4] 吳寶林, 曹喜濱, 任子武, “一種長期穩定的衛星編隊隊形最佳化設計方法”, 航空學報, Vol. 28, No. 1, 2007, pp. 167-172.

[5] 吳寶林, 曹喜濱, 攝動橢圓參考軌道的相對運動狀態轉移方程, 宇航學報, Vol. 26, No. 6, 2005, pp. 702-706.

[6] 吳寶林, 曹喜濱, 基於模型預測的衛星編隊隊形機動控制, 吉林工業大學學報工學版，2007年第一期, pp. 218-223

[7] 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.

[8] 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.

[9] Qiang Shen, Chengfei Yue, Cher Hiang Goh, Baolin Wu, and Danwei Wang, Rigid-body attitude stabilization with attitude and angular rate constraints, Automatica, 2018.

[10] 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

[11] 耿雲海, 劉偉星, 吳寶林, 轉動慣量未知的再入飛行器姿態容錯控制,宇航學報, 已錄用.

會議論文

[1] Baolin Wu, Xibin Cao, Satellite Formation Keeping Using Robust Constrained Model Predictive Control, 1st International Symposium on Systems and Control in Aerospace and Astronautics, 19-21, Jan. 2006.

[2] 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.

[3] 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.

[4] 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.

[5] Baolin Wu, Eng Kee Poh, Wang, Danwei; Xu, Guangyan, Satellite Formation Keeping via Real-Time Optimal Control and Iterative Learning Control, IEEE Aerospace conference, Big Sky, MT, USA, 7-14 March 2009.

[6] Xu, Guangyan; Poh, Eng Kee; Wang, Danwei; Baolin Wu, In-Plane Satellite Formations in Eccentric Orbits under J2 Perturbation, IEEE Aerospace conference, Big Sky, MT, USA, 7-14 March 2009.

[7] 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.

[8] Baolin Wu, Eng Kee Poh, Wang, Danwei, Decentralized Control for Satellite Formation Using Local Relative Measurements Only, the 8th IEEE International Conference on Control & Automation. Xiamen, China, June 9-11, 2010.

[9] 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.

[10] 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.

[11] 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.

[12] 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.

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

[14] 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.