吴宝林

基本信息 科学研究 教育教学 学术专著 学术论文 招生信息 English 新页签 ... 招生信息 en English 新页签 新建主栏目 基本信息 名称 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。2023年入选Elsevier发布的航空航天大领域全球前2%顶尖科学家榜单，中国大陆地区266名科学家入选，本人排名73名。 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，航天器在轨服务与空间攻防等领域的研究。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55篇SCI期刊论文和7篇一级学报论文，其中7篇论文发表在航空航天国际顶级期刊Journal of Guidance, Control and Dynamics和12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。 近年深度参与我国国之重器某空天飞机的研制，主要负责其轨道控制算法设计与仿真，姿态控制算法设计与仿真，任务设计分析与仿真，以及相关软件开发等研究工作。 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 名称 时间 工作经历 2011.2-2013.5 姿态控制工程师, ST Electronics (Satellite Systems) Pte Ltd, Singapore 2013.5-2013.12 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 名称 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 名称 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 空间攻防、态势感知中的姿轨控制 科研项目 名称 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。作为分系统负责人参加绕月卫星编队、xxx型号编队控制、超低轨电推进某型号卫星等工程项目。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。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)". 本人作为分系统负责人参与的五个工程项目简介如下： 国之重器某空天飞机轨道控制与任务分析 近年来本人参与我国国之重器某空天飞机的轨道控制系统、姿态控制系统，及任务设计与仿真分析等研究。主要负责各种轨道控制算法研究与仿真分析，各种姿态控制模式算法设计与仿真，各作战模式设计和效能评估，各种任务设计与仿真分析以及软件开发。 绕月卫星编队 该项目是世界上第一个月球轨道航天器编队项目，由哈工大卫星技术研究所负责研制。项目来源于探月工程嫦娥四号中继星搭载任务。该项目任务目标利用嫦娥四号中继卫星运载火箭剩余能力，研制并搭载发射两颗微卫星，以近距离绕月编队飞行的形式构建分布式超长波天文观测微卫星系统。项目研究经费5800万元。申请人作为编队控制分系统负责人参与该项目，编队控制是该项目的两个最主要关键技术之一。卫星于2018成功发射。 xx卫星编队控制系统 该项目是我国第一个立项的航天器编队飞行任务型号，项目目标是研制两颗卫星形成地球低轨道近距离编队，用于分布式测绘。 卫星编队控制系统项目为xx型号的一个分系统，也是该型号任务的最重要的关键技术。申请人负责xx卫星编队控制系统研制，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。两颗卫星于2019成功发射。 超低轨电推进卫星 该卫星是我国首颗超低轨道xxx飞行卫星，本人目前负责该型号卫星的姿态与轨道控制系统研究。该系统的关键技术包括挠性卫星的敏捷机动和高精度轨道控制。 TeLEOS-1卫星姿态确定与控制系统 本人博士毕业后于2011.2-2013.5期间在新加坡一家卫星研发单位“ST Electronics (Satellite Systems) Pte Ltd”担任卫星姿态控制工程师。主要负责卫星TeLEOS-1的姿态确定与控制算法设计与测试。TeLEOS-1是新加坡首颗自主研发的光学遥感商业卫星。TeLEOS-1于2015年12月由印度PSLV火箭成功发射。该卫星对姿态系统要求很高。一方面，为了提高成像分辨率，要求卫星具有高指向精度和高稳定度。另一方面，该卫星具备多种灵巧成像模式，包括多目标成像、拼接成像和非沿星下点轨迹成像。 本人和研发团队与绕月微卫星合影 团队成员 名称 本人指导毕业博士8人，毕业硕士15人，在读博士生9人，在读硕士生7人。课题组内科研气氛活跃，组内讨论热烈，指导的学生已发表一系列高水平论文，取得了丰硕的研究成果。 已毕业博士生: 1，张志刚，论文题目：绳系InSAR系统构形展开与波束同步控制研究，2016年毕业。 2，侯志立，论文题目：卫星快速姿态机动过程中SGCMG奇异规避方法研究，2017年毕业 3，曾奎，论文题目：基于形状曲线逼近法的小推力航天器轨迹设计，2018年毕业， 4，郭继唐，论文题目：基于控制力矩陀螺群的航天器姿态控制方法研究，2020年毕业 5，易涛，论文题目：航天器姿态机动中控制力矩陀螺群操纵方法研究，2022年毕业。 6，赵显，论文题目：基于磁轴承连接的旋扫成像航天器动力学与控制研究，2022年毕业。 7，刘伟星，论文题目：基于多细胞结构的航天器姿态接管控制，2022年毕业。 8，许闯，论文题目：有向通讯结构下多航天器系统分布式固定和预设时间姿态协同控制，2022年毕业。 9，胡雅博, 论文题目: 挠性卫星姿态控制与振动抑制, 2023年毕业。 10，宁凯，论文题目: 挠性卫星姿态控制与振动抑制, 2024年毕业。 在读博士生: 1，史明月(2020-至今)，研究方向：通信约束下的航天器姿态控制与力矩分配 2，王孟磊(2020-至今)，研究方向：航天器姿态接管控制中的目标航天器状态感知与控制 3，林子杰(2021-至今)，研究方向：基于微纳卫星集群的航天器抵近控制与柔顺化附着控制 4，马嘉宏(2021-至今)，研究方向：超低轨道航天器姿态与轨道控制。 5，伍攀峰(2021-至今)，研究方向：航天器星务管理系统。 6，孙兆博（2022-至今），研究方向：事件驱动模型预测控制及其在航天器编队构形控制中的应用。 7，张小翔（2022-至今），研究方向：多对多空间攻防制导与控制 8，刘阳，（2023-至今），研究方向：基于微纳卫星的空间态势感知任务规划与控制 9，陈俊宇，（2024-至今），研究方向：大规模航天器编队构形协同控制 10，郭超（2023-至今），研究方向：基于微纳卫星群的空间攻防中姿态轨道控制问题 ， 在读硕士生: 1，董雨洋 2，史佳新 3，刘辰宇 4，郭艳冰 5，侯佳伦 6，邓传锐晨 学术组会现场照片1 学术组会现场照片2 游玩帽儿山（2021年5月） 香炉山之行（2022年6月） 红星水库烧烤（2023.6） 航天器编队飞行理论与实践（本科生创新研修课）（2020-至今） 名称 航天器的空间应用已从单星迈向编队组网化，它是伴随现代小卫星技术快速发展而提出的一种创新应用模式，能够充分发挥小卫星的应用效能。通过多颗小卫星按一定的空间构型协同工作可以实现大卫星的功能或完成传统单颗大卫星难以实现的空间任务，满足特殊任务需求、降低风险和成本。本课程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；课程内容包括：航天器间相对动力学基础；航天器空间编队构形设计；航天器空间编队构形初始化、维持和重构控制理论与方法等内容。 航天通用软件应用-STK（本科生课程）（2019-至今） 名称 对于航天器任务分析、轨道设计与控制、姿态控制，STK是最佳的数学仿真工具。该课程是培养从事航天器总体设计、姿轨控领域研究和工程设计专业人才的重要组成部分。该课程讲授STK的基本模块、可见性分析、姿态控制模块、覆盖分析、链路模块、轨道机动模块和外部接口等模块的使用方法；让学生掌握针对航天器任务分析，轨道设计与控制、姿态控制等，具备使用STK软件进行分析、设计与数学仿真能力。 飞行器系统仿真与CAD（研究生课程）（2022-至今） 名称 飞行器系统仿真与CAD课程是飞行器设计学科的一门研究生学科核心课。该课程是培养从事航天器总体设计、姿轨控领域研究和工程设计专业人才的重要组成部分。Matlab和STK软件是飞行器系统最佳的任务分析与仿真工具。通过本课程的学习，使学生了解和掌握基于STK的飞行器任务分析、飞行器轨道设计，轨道控制、姿态控制和飞行器编队构形设计与控制等设计与仿真技术与方法。培养学生基于STK进行航天器设计与仿真的能力。 航天器编队飞行理论 (本科生课程)（2015-2020） 名称 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 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 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。 宣传单 名称 SCI期刊学术论文(第一作者或通信作者为本人) 名称 Journal of Guidance, Control and Dynamics: [1] 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. [2] 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. [3] 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. [4] Baolin Wu*, Spacecraft Attitude Control with Input Quantization, Journal of Guidance, Control, and Dynamics, Vol. 39, No. 1, 2016, pp. 176-180. [5] 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. [6] 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. [7] Zijie Lin, Baolin Wu*, Danwei Wang, Occlusion Avoidance in Image-Based Control of Multiple Spacecraft, Journal of Guidance, Control, and Dynamics, 2024, Online Published. IEEE Transactions: [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, pp. 1020-1028. [2]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. [3] 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 [4] 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. [5] 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. [6] 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. [7] 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. [8] 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. [9] 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 [10] 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. [11] 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 [12] Menglei Wang, Baolin Wu*, Yunhai Geng and Danwei Wang, Distributed Approximate Optimal Attitude Control of Combined Spacecraft with Parameters Identification, IEEE Transactions on Aerospace and Electronic Systems, Online Published Acta Astronautica: [1]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 [2]Baolin Wu, D Wang, EK Poh, Decentralized sliding-mode control for spacecraft attitude synchronization under actuator failures, Acta Astronautica 105 (1), 333-343, 2014 [3] Jinxiu Zhang, Zhigang Zhang, Baolin Wu*, Decentralized adaptive sliding mode control for beam synchronization of tethered InSAR system, Acta Astronautica 127, 57-66, 2016. [4]Xibin Cao, Baolin Wu*, Robust Spacecraft Attitude Tracking Control Using Hybrid Actuators with Uncertainties, Acta Astronautica, Vol. 136, 2017, pp. 1-8. [5] Zhili Hou, Yunhai Geng and Baolin Wu*, Spacecraft Angular Velocity Trajectory Planning for SGCMG Singularity Avoidance, Acta Astronautica,Vol. 151, 2018, pp. 284-295. [6]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. [7] 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. [8] 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 [9] Junyu Chen, and Baolin Wu*, Distributed safe trajectory optimization for large-scale spacecraft formation reconfiguration, Acta Astronautica, Accepted. Aerospace Science and Technology: [1] 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 [2] 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 [3]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. [4]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. [5]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. [6] 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. [7]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: [1] 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. [2] 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: [1] 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. [2] 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. [3] 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. [4] 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: [1] 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 [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, Vol. 62, No. 3, Aug. 2018, 593-613. [3] 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. [4] 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. [5] 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: [1] 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. [2]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. [3] Chuang Xu, Daniel Zelazo, Baolin Wu*, Bearing-Based Formation Control of Second-Order Multi-Agent Systems with Bounded Disturbances. Online Published. Others: [1] 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. [2] 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. [3]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. [4], 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 [5] 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. [6]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 名称 [1]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. [2]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. [3]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. [4]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. [5]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. [6]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 [7] 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 [8]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 [9]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. [10]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. [11]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. [12]Qiang Shen, Chengfei Yue, Cher Hiang Goh, Baolin Wu, and Danwei Wang, Rigid-body attitude stabilization with attitude and angular rate constraints, Automatica, 2018. [13]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 名称 [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 名称 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 招生信息 名称 招收航空宇航、控制理论与工程、数学等相关学科的硕士和博士研究生。每年招收博士生1-2名，硕士生3-4名。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、构形设计与构形控制 航天器集群路径规划与控制 航天器轨道优化与控制 控制力矩陀螺操纵律设计等 Baolin WU 名称 Full Professor, PhD Supervisor, Research Center of Satellite Technology, School of Astronautics, Harbin Institute of Technology. I have published 43 SCI indexed papers and 1 book "Satellite Formation Flying"in the field of Aerospace GNC. 3-4 master students and 1-2 PhD students vacancies are avaialbe every year. Welcome you to join my research group! Please contact me by wubaolin@hit.edu.cn Education 名称 1999.9-2003.6, Bachelor, Harbin Institute of Technology, Flight Vehicle Design, School of Astronautics. 2003.9-2005.6, Master, Harbin Institute of Technology, Flight Vehicle Design, Research Centre of Satellite Technology,School of Astronautics. 2007.1-2011.8, PhD, Nanyang Technological University, Singapore, Division of Control and Instrumentation, School of Electrical and Electronic Engineering. Working Experience 名称 2011.2-2013.6, Attitude Control Engineer, ST Electronics (Satellite Systems) Pte Ltd, Singapore. 2013.6-2013.12, Research Fellow, School of EEE, Nanyang Technological University, Singapore. 2014.1-2019.12, Associate Professor, Research Center of Satellite Technology, School of Astronautics, Harbin Institute of Technology. 2019.12-Now, Full Professor, Research Center of Satellite Technology, School of Astronautics, Harbin Institute of Technology. Research Interest 名称 Attitude control of spacecraft Attitude Synchronization of spacecraft Trajectory optimization of spacecraft Formation control of spacecraft CMG steering law design Orbit control of spacecraft Selected Publication List 名称 Journal of Guidance, Control and Dynamics: [1] 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. [2] 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. [3] 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. [4] Baolin Wu*, Spacecraft Attitude Control with Input Quantization, Journal of Guidance, Control, and Dynamics, Vol. 39, No. 1, 2016, pp. 176-180. [5] 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. [6] 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: [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, pp. 1020-1028. [2]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. [3] 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 [4] 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. [5] 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. [6] Chuang Xu, Baolin Wu*, and Danwei Wang, Distributed Prescribed-Time Attitude Coordination for Multiple Spacecraft with Actuator Saturation under Directed Grap. IEEE Transactions on Aerospace and Electronic Systems. DOI: 10.1109/TAES.2021.3135484. [7] 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, Accepted. Acta Astronautica: [1]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 [2]Baolin Wu, D Wang, EK Poh, Decentralized sliding-mode control for spacecraft attitude synchronization under actuator failures, Acta Astronautica 105 (1), 333-343, 2014 [3] Jinxiu Zhang, Zhigang Zhang, Baolin Wu*, Decentralized adaptive sliding mode control for beam synchronization of tethered InSAR system, Acta Astronautica 127, 57-66, 2016. [4]Xibin Cao, Baolin Wu*, Robust Spacecraft Attitude Tracking Control Using Hybrid Actuators with Uncertainties, Acta Astronautica, Vol. 136, 2017, pp. 1-8. [5] Zhili Hou, Yunhai Geng and Baolin Wu*, Spacecraft Angular Velocity Trajectory Planning for SGCMG Singularity Avoidance, Acta Astronautica,Vol. 151, 2018, pp. 284-295. [6]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. [7] 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. Aerospace Science and Technology: [1] 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 [2] 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 [3]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. [4]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. [5]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. [6] 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. [7]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. Journal of Aerospace Engineering: [1] 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. [2] 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: [1] 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. [2] 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. [3] Xian Zhao, Yunhai Geng, Baolin Wu*, Chao Yuan, Dynamics and Adaptive Backstepping Control of Multibody Spacecraft Connected with Active Magnetic Bearing, In Press. Advances in Space Research: [1] 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 [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, Vol. 62, No. 3, Aug. 2018, 593-613. [3] 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. International Journal of Robust and Nonlinear Control: [1] 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. [2]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 ControlIn Press. Others: [1] 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. [2] 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. [3]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. [4], 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 [5] 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. [6]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, In Press. Contact Information 名称 wubaolin@hit.edu.cn wuba0001@e.ntu.edu.sg 名称 已毕业博士生 1，张志刚，论文题目：绳系InSAR系统构形展开与波束同步控制研究，2016年毕业。 2，侯志立，论文题目：卫星快速姿态机动过程中SGCMG奇异规避方法研究，2017年毕业， 目前就职于清华大学深圳研究生院。 3，曾奎，论文题目：基于形状曲线逼近法的小推力航天器轨迹设计，2018年毕业，目前就职于武汉航天四院。 4，郭继唐，论文题目：基于控制力矩陀螺群的航天器姿态控制方法研究，2020年毕业，目前就职于航天五院钱学森实验室。 5，易涛，论文题目：航天器姿态机动中控制力矩陀螺群操纵方法研究，2022年毕业，目前就职于航天八院509所。 6，赵显，论文题目：基于磁轴承连接的旋扫成像航天器动力学与控制研究，2022年毕业，目前就职于航天五院502所。 在读博士生 1, 许 闯(2018-至今)，研究方向：航天器姿态协同控制 2，刘伟星(2017-至今)，研究方向：细胞化航天器姿态控制与力矩分配 3，胡雅博(2018-至今)，研究方向：挠性卫星姿态控制与振动抑制 4，宁凯(2019-至今)，研究方向：基于事件驱动的航天器姿态轨道控制 5，史明月(2020-至今)，研究方向：通信约束下的航天器姿态控制与力矩分配 6，王孟磊(2020-至今)，研究方向：航天器姿态接管控制中的目标航天器状态感知与控制 7，林子杰(2021-至今)，研究方向：基于微纳卫星集群的航天器抵近控制与柔顺化附着控制 8，马嘉宏(2021-至今)，研究方向：超低轨道航天器姿态与轨道控制。