基本信息科学研究教育教学学术专著学术论文
基本信息
吴宝林，(校青年拔尖)副教授，博士生导师，1983年出生，哈尔滨工业大学航天学院卫星技术研究所。

从事航天器编队相对动力学与控制和航天器姿态控制与协同等领域的研究。以第一作者或通信作者共发表23篇SCI期刊论文和5篇一级学报论文，其中6篇论文发表在航空航天国际顶级期刊Journal of Guidance, Control and Dynamics和IEEE Transactions on Aerospace and Electronic Systems上。在Springer上出版英文专著一本《Satellite Formation Flying》。

以负责人身份主持如下项目：国家自然科学基金面上项目、国家自然科学基金青年基金、哈尔滨工业大学青年拔尖副教授选聘计划、哈工大重点实验室开放基金等。作为技术骨干参加两个重要型号任务，以及国家自然科学基金重大专项。其中，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，于2018年5月发射。本人负责负责该项目关键技术研究，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。另外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。

欢迎各位海内外同仁联系交流，欢迎各位同学报考硕博研究生！


工作经历
时间工作经历
2011.2-2013.5姿态控制工程师, ST Electronics (Satellite Systems) Pte Ltd, Singapore
2013.6-2013.12博士后，新加坡南洋理工大学
2014.1-2018.04(校青年拔尖)副教授，硕士生导师，哈尔滨工业大学
2018.04-至今(校青年拔尖)副教授，博士生导师，哈尔滨工业大学



教育经历
1999年-2003年, 本科，哈尔滨工业大学，航天学院，飞行器设计专业2003年-2005年, 硕士，哈尔滨工业大学，航天学院，卫星技术研究所2007年-2011年, 博士，南洋理工大学(新加坡)，电机与电子工程学院


研究领域
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

团队成员
本人指导和协助指导的博士生和硕士生共计20来人。本人主持每周的学术组会，参加人数20多人，组会讨论热烈，气氛活跃。


科研项目
本人负责国家自然科学基金、校青年拔尖人才选聘计划等项目。作为技术骨干参加绕月、xx型号编队控制等工程项目。

我国仅有的两个航天器编队型号项目的编队控制系统都是本人主要负责研究，都将于2018发射。第一个项目是绕月卫星编队，该项目将国际首次实现月球轨道近距离航天器编队。项目来源于嫦娥四号搭载任务。本人负责该项目的两个关键技术之一的编队控制系统研究。

第二个项目是xx型号编队控制系统研制。该项目是我国第一个立项的航天器编队型号项目。本人主要负责该项目的编队构形初始化、构形重构、构形维持的算法设计与软件编写及测试。

另外，本人还负责自然基金面上项目“大规模微纳航天器集群构形控制与姿态协同(2019-2022)”以及青年基金项目"分布式空间太阳能电站的队形设计与协同控制(2016-2018)".



航天器编队飞行理论 (本科生课程)
通过本课程，让本科生了解航天器系统的最新发展方向——航天器编队飞行的相关概念、理论与方法，涵盖了航天器编队飞行的概念、发展现状以及产生的背景；航天器间相对动力学基础；航天器空间编队构形确定；航天器间相对状态测量与确定；航天器空间编队构形初始化、维持和重构理论与方法等内容


招生信息
招收航空宇航和控制等相关学科的硕士和博士研究生。主要招生方向有
航天器姿态控制航天器姿态协同控制航天器编队相对动力学与控制轨道优化与控制等。

学术专著

出版物名称Satellite Formation Flying

作者Danwei Wang; Baolin Wu; Eng Kee Poh

出版时间,完成时间2017.01

出版社Springer

简单介绍该书系统的介绍了卫星编队的动力学建模，构形设计，构形控制以及姿态协同。

SCI期刊学术论文(第一作者或通信作者为本人)

[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, 2018.

[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 Directed Communication 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 via Iterative 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, Vol. 54, No. 5, 2018, pp. 2509-2525.

[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 Yunhua Wu, Smooth Time-Optimal Attitude Control of Spacecraft, Part G. Journal of Aerospace Engineering, Vol. 62, No. 3, 2018, pp593-613.

[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, In Press.

[22] Zhili Hou, Yunhai Geng and Baolin Wu, Spacecraft Angular Velocity Trajectory Planning for SGCMG Singularity Avoidance, Acta Astronautica,Vol. 151, 2018, pp. 284-295.

[23] Chuang Xu, Baolin Wu, Xibin Cao and Yingchun Zhang, Distributed Adaptive Event-Triggered Control for Attitude Synchronization of Multiple Spacecraft, Nonlinear Dynamics, In Press.


其它期刊论文

[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,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.

[3]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.

[4]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.

[5]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.

[6]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

[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.

会议论文

[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.

[15] Chuang Xu, Baolin Wu, and Dawei Wang, Smooth Rapid Attitude Maneuver Control of Spacecraft, The 30th Chinese Control and Decision Conference. 2018 Shen Yang.


本人学术论文链接
1， 谷歌学术个人主页

http://scholar.google.com/citations?user=D6fP9tEAAAAJ&hl=en&oi=ao

or

https://xue.glgoo.com/citations?user=D6fP9tEAAAAJ&hl=zh-CN&oi=ao

2, ResearchGate 个人主页

https://www.researchgate.net/profile/Baolin_Wu2