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个人简介

吴宝林,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。 从事航天器编队集群相对动力学与控制、航天器姿态控制与协同,航天器在轨服务等领域的研究。系统性的解决了地球扁率摄动下的编队动力学与控制相关理论问题,提出了多种有效的高精度姿态控制与姿态协同控制方法。以第一作者或通信作者共发表53篇SCI期刊论文和7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11篇论文发表在航空航天IEEE Transactions 会刊上。 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。作为分系统负责人参加三个重要型号任务、国家自然科学基金重大专项以及民用航天等项目。其中,作为编队控制分系统负责人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”,该项目目标是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xxxx/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分布式测绘的航天器编队飞行任务型号,双星于2019年成功发射。 目前负责我国国之重器某空天飞机的轨道控制,姿态控制,任务分析等研究工作。另外负责我国超低轨电推进某型号卫星的姿态与轨道控制系统等研究。 工作经历 2011.2-2013.5 姿态控制工程师, ST Electronics (Satellite Systems) Pte Ltd, Singapore 2013.5-2013.12 博士后,新加坡南洋理工大学 2014.1-2019.12 (校青年拔尖)副教授,哈尔滨工业大学 2018.04-至今 博士生导师,哈尔滨工业大学 2019.12-至今 教授,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

航天器编队集群相对动力学与控制 航天器姿态控制与姿态协同 航天器轨道控制与优化 航天器在轨服务中的姿态轨道控制 控制力矩陀螺操纵律设计与力矩分配

近期论文

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Journal of Guidance, Control and Dynamics: 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. Baolin Wu, Danwei Wang,* and Eng Kee 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. Baolin Wu, Danwei Wang*, and Eng Kee Poh, High-Precision Satellite Attitude Tracking Control via Iterative Learning Control, Journal of Guidance, Control, and Dynamics, Vol. 38, No. 3, 2015, Pages: 528-534. Baolin Wu*, Spacecraft Attitude Control with Input Quantization, Journal of Guidance, Control, and Dynamics, Vol. 39, No. 1, 2016, pp. 176-180. Hu Yabo, Geng Yunhai, Wu Baolin*, Wang Danwei, Flexible Spacecraft Vibration Suppression by Distributed Actuators, Journal of Guidance, Control, and Dynamics, Vol. 43, No. 11, 2020, pp. 2141-2147. DOI: doi/abs/10.2514/1.G005190. Weixing Liu, Geng Yunhai, Wu Baolin*, and James D. Biggs, Distributed Constrained Control Allocation for Celluralized Spacecraft Attitude Control System, Journal of Guidance, Control, and Dynamics, Vol. 45, No.2, 2021, pp.385-393. IEEE Transactions: 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, pp. 1020-1028. 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. Chuang Xu, Baolin Wu*, Danwei Wang and Yingchun Zhang, Distributed Fixed-Time Output-Feedback Attitude Consensus Control for Multiple Spacecraft. IEEE Transactions on Aerospace and Electronic Systems. Vol. 56, No. 6, pp. 4779-4795, 2020. DOI: 10.1109/TAES.2020.3003119 Liu Weixing, Geng Yunhai, Wu Baolin*, Wang Danwei,Neural-Network-based Adaptive Event-triggered Control for Spacecraft Attitude Tracking, IEEE Transactions on Neural Networks and Learning Systems, Vol. 31, No. 10, 2020, pp. 4015-4024. Hu Yabo, Geng Yunhai, Wu Baolin*, Wang Danwei, Model-Free Prescribed Performance Control for Spacecraft Attitude Tracking, IEEE Transactions on Control Systems Technology, 2021, Vol. 29, No.1, pp.165-179, DOI: 10.1109/TCST.2020.2968868. Chuang Xu, Baolin Wu*, and Danwei Wang, Distributed Prescribed-Time Attitude Coordination for Multiple Spacecraft with Actuator Saturation under Directed Graph. IEEE Transactions on Aerospace and Electronic Systems. Vol. 58, No. 4, 2022, pp. 2660-2672. DOI: 10.1109/TAES.2021.3135484. Menglei Wang, Geng Yunhai, Wu Baolin*, Wang Danwei, Distributed Adaptive Attitude Takeover Control of Failed Spacecraft with Parameters Identification, IEEE Transactions on Control Systems Technology, March, 2023, Vol. 31, No. 2, pp. 897-904. DOI:10.1109/TCST.2022.3187921. Hongyi Xie, Baolin Wu*, and Franco Bernelli-Zazzera,High Minimum Inter-execution Time Sigmoid Event-triggered Control for Spacecraft Attitude Tracking with Actuator Saturation, IEEE Transactions on Automation Science and Engineering, DOI:10.1109/TASE.2022.3179896. Zijie Lin, Baolin Wu*, and Danwei Wang, Specific Tracking Control of Rotating Target Spacecraft under Safe Motion Constraints, IEEE Transactions on Aerospace and Electronic Systems, 2023, 59(3): 2422-2438, DOI 10.1109/TAES.2022.3214799 Kai Ning, Baolin Wu*, and Danwei Wang, Velocity Observer-Based Event-Triggered Adaptive Fuzzy Attitude Takeover Control of Spacecraft with Quantized Quaternion, IEEE Transactions on Aerospace and Electronic Systems, Vol. 59, No. 4, 2023, 4168-4179. DOI: 10.1109/TAES.2023.3237127. Baolin Wu, Keyu Chen, Danwei Wang, Yuxiang Sun, Spacecraft Attitude Takeover Control by Multiple Microsatellites Using Differential Game, IEEE Transactions on Control of Network Systems, Accepted.DOI: 10.1109/TCNS.2023.3290082 Acta Astronautica: Baolin Wu, X Cao, Z Li, Multi-objective output-feedback control for microsatellite attitude control: An LMI approach, Acta Astronautica 64 (11), 1021-1031, 2009 Baolin Wu, D Wang, EK Poh, Decentralized sliding-mode control for spacecraft attitude synchronization under actuator failures, Acta Astronautica 105 (1), 333-343, 2014 Jinxiu Zhang, Zhigang Zhang, Baolin Wu*, Decentralized adaptive sliding mode control for beam synchronization of tethered InSAR system, Acta Astronautica 127, 57-66, 2016. Xibin Cao, Baolin Wu*, Robust Spacecraft Attitude Tracking Control Using Hybrid Actuators with Uncertainties, Acta Astronautica, Vol. 136, 2017, pp. 1-8. Zhili Hou, Yunhai Geng and Baolin Wu*, Spacecraft Angular Velocity Trajectory Planning for SGCMG Singularity Avoidance, Acta Astronautica,Vol. 151, 2018, pp. 284-295. Baolin Wu*, Chuang Xu, and Yingchun Zhang, Decentralized Adaptive Control for Attitude Synchronization of Multiple Spacecraft via Quantized Information Exchange, Acta Astronautica, Oct, 2020, Vol. 175, pp.57-65. Chuang Xu, Baolin Wu*, and Danwei Wang, Distributed Dynamic Event-Triggered Adaptive Attitude Consensus Control of Multiple Spacecraft. Acta Astronautica, Volume 196, July 2022, Pages 220-230. Xiaoxiang Zhang, Yunhai Geng, and Baolin Wu*,Approaching and Pointing Tracking Control for Tumbling Target Under Motion Constraints, Acta Astronautica, Volume 209, August 2023, Pages 6-20. PP.6-20 Junyu Chen, and Baolin Wu*, Distributed safe trajectory optimization for large-scale spacecraft formation reconfiguration, Acta Astronautica, Accepted. Aerospace Science and Technology: Xibin Cao, Baolin Wu*, Indirect adaptive control for attitude tracking of spacecraft with unknown reaction wheel friction, Aerospace Science and Technology 47, 493-500, 2015 Baolin Wu*, Xibin Cao, Lei Xing, Robust adaptive control for attitude tracking of spacecraft with unknown dead-zone, Aerospace Science and Technology 45, 196-202 2015 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. 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. Jitang Guo, Yunhai Geng, Baolin Wu*, and Xianren Kong, Manifold Path Selection Steering Law for Pyramid-type Single-gimbal Control Moment Gyros, Aerospace Science and Technology, Vol. 106, Nov 2020, 106207. Chuang Xu, Baolin Wu*, Danwei Wang and Yingchun Zhang, Distributed Prescribed-Time Attitude Cooperative Control for Multiple Spacecraft . Aerospace Science and Technology, 113,2021: 106699. Tao Yi, Yunhai Geng, and Baolin Wu*,Robust Gimbal Reorientation Singularity-Avoidance Steering Strategy for Regular Pentagonal Pyramid Configuration with Two Control Moment Gyroscopes Failed . Aerospace Science and Technology, 119(2021)107174, 1-14. Journal of Aerospace Engineering: Baolin Wu*, Guangyan Xu, Xibin Cao, Relative Dynamics and Control for Satellite Formation: Accommodating J2 Perturbation, Journal of Aerospace Engineering, Vol. 29, No. 4, July 2016, 04016011. Zhili Hou, Yunhai Geng and Baolin Wu*, New Set of Attitude Parameters Dedicated to Relative Attitude Maneuvers, Journal of Aerospace Engineering, 2020, 33(4): 04020022. DOI: 10.1061/(ASCE)AS.1943-5525.0001137. Part G: Journal of Aerospace Engineering: Baolin Wu, Danwei Wang, Eng Kee Poh, Energy-optimal low-thrust satellite formation manoeuvre in presence of J2 perturbation, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 225, No. 9, 2011, pp. 961-968. Yabo Hu, Baolin Wu*, Yunhai Geng and Yunhua Wu, Smooth Time-Optimal Attitude Control of Spacecraft, Proceedings of the Institution of Mechanical Engineers, Part G. Journal of Aerospace Engineering, Vol. 62, No. 3, 2018, pp593-613. Xian Zhao, Yunhai Geng, Baolin Wu*, Chao Yuan, Dynamics and Adaptive Backstepping Control of Multibody Spacecraft Connected with Active Magnetic Bearing, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2022, Vol. 236, No. 12, pp. 2508–2522. Mingyue Shi, Baolin Wu, and Chuang Xu, Predefined-Time Attitude Takeover Control of Spacecraft with Quantized States, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2023, Vol. 237, No. 10, pp. 2341-2352, August DOI:10.1177/09544100231153318. Advances in Space Research: 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 Kui Zeng, Baolin Wu*, and Yunhai Geng, Two-Phase Shaping Approach to Low-Thrust Trajectories Design Between Coplanar Orbits, Advances in Space Research, 2018, Vol. 62, No. 3, Aug. 2018, 593-613. Ning Kai, Baolin Wu*, and Chuang Xu , Event-Triggered Adaptive Fuzzy Attitude Takeover Control of Spacecraft, Advances in Space Research, Vol. 67, No. 6, March 2021, pp. 1761-1772. Mingyue Shi, Baolin Wu*, and Danwei Wang, Neural-Network-Based Adaptive Quantized Attitude Takeover Control of Spacecraft by Using Cellular Satellites, Advances in Space Research, Volume 70, Issue 7, 1 October 2022, Pages 1965-1978. Chuang Xu, Baolin Wu*, Danwei Wang and Fei Han, Distributed Prescribed-Time Attitude Consensus for Multiple Spacecraft via Quantized Communication. Advances in Space Research, Volume 71, Issue 10, 15 May 2023, Pages 4302-4314. https://doi.org/10.1016/j.asr.2022.12.053 International Journal of Robust and Nonlinear Control: Baolin Wu, Danwei Wang, Eng Kee Poh, Decentralized sliding‐mode control for attitude synchronization in spacecraft formation, International Journal of Robust and Nonlinear Control 23 (11), 1183-1197, 2013. Xian Zhao, Yunhai Geng, Tao Yi, Baolin Wu*, Weixing Liu, Composite Adaptive Backstepping Controller for Variable Speed Rotating Scan Optical Spacecraft, International Journal of Robust and Nonlinear Control, 2022;32(6):4008-4037. Chuang Xu, Daniel Zelazo, Baolin Wu*, Bearing-Based Formation Control of Second-Order Multi-Agent Systems with Bounded Disturbances. Online Published. Others: Baolin Wu*, Xibin Cao, Decentralized Control for Spacecraft Formation in Elliptic Orbits, Aircraft Engineering and Aerospace Technology, Vol. 90, No. 1,· 2018,pp.166–174. Chuang Xu, Baolin Wu*, Xibin Cao and Yingchun Zhang, Distributed Adaptive Event-Triggered Control for Attitude Synchronization of Multiple Spacecraft, Nonlinear Dynamics, March 2019, Vol. 95, No. 4, pp. 2625-2638. Tao Yi, Yunhai Geng, and Baolin Wu*, Singularity Radius Gradient-Based Rapid Singularity-Escape Steering Law for SGCMGs, Chinese Journal of Aeronautics, Vol. 33, No. 10, Oct. 2020, pp. 2728-2742. Chuang Xu, Baolin Wu*, Danwei Wang, Yingchun Zhang, Decentralized Event-Triggered Finite-Time Attitude Consensus Control of Multiple Spacecraft under Directed Graph,Journal of the Franklin Institute, 358 (2021) 9794–9817 Hongyi Xie, Baolin Wu*, and Weixing Liu, Adaptive neural network model-based event-triggered attitude tracking control for spacecraft, International Journal of Control, Automation and Systems, Vol. 19, pp.172-185, 2021. Xian Zhao, Yunhai Geng, Chao Yuan, and Baolin Wu*, An Unscented Kalman Filter Based Iterative Learning Controller for Multibody Rotating Scan Optical Spacecraft, Transactions of the Institute of Measurement and Control, 2022, Vol. 44(12) 2418–2433. 其它期刊论文 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, 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. 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. 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, 2018,39(06),683-689. 许闯,吴宝林,输入饱和下多航天器分布式固定时间输出反馈姿态协同控制,航空学报,已录用. DOI: 10.7527/S1000-6893.2022.27465 刘伟星, 耿云海,吴宝林, 细胞化卫星分布式角动量平衡力矩分配算法,宇航学报, 2023, 44 (1): 62-72. DOI: 10.3873/j.issn.1000-1328.2023.01.007 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 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. 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. Qiang Shen, Chengfei Yue, Cher Hiang Goh, Baolin Wu, and Danwei Wang, 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 会议论文 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. 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, IEEE Aerospace conference, Big Sky, MT, USA, 7-14 March 2009. 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. 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, the 8th IEEE International Conference on Control & Automation. Xiamen, China, June 9-11, 2010. 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. Chuang Xu, Baolin Wu, and Dawei Wang, Smooth Rapid Attitude Maneuver Control of Spacecraft, The 30th Chinese Control and Decision Conference. 2018 Shen Yang.

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