吳寶林

負責國家自然科學基金、校青年拔尖人才選聘計劃等項目。作為分系統負責人蔘加繞月衞星編隊、xxx型號編隊控制、超低軌電推進某型號衞星等工程項目。主要負責我國僅有的兩個航天器編隊型號項目的編隊控制系統研究。另外，還負責自然基金面上項目“大規模微納航天器集羣構形控制與姿態協同(2019-2022)”以及青年基金項目"分佈式空間太陽能電站的隊形設計與協同控制(2016-2018)". 作為分系統負責人蔘與的四個工程項目簡介如下：

該項目是世界上第一個月球軌道航天器編隊項目，由哈工大衞星技術研究所負責研製。項目來源於探月工程嫦娥四號中繼星搭載任務。該項目任務目標利用嫦娥四號中繼衞星運載火箭剩餘能力，研製並搭載發射兩顆微衞星，以近距離繞月編隊飛行的形式構建分佈式超長波天文觀測微衞星系統。項目研究經費5800萬元。申請人作為編隊控制分系統負責人蔘與該項目，編隊控制是該項目的兩個最主要關鍵技術之一。衞星於2018成功發射。

該項目是我國第一個立項的航天器編隊飛行任務型號，項目目標是研製兩顆衞星形成地球低軌道近距離編隊，用於分佈式測繪。 衞星編隊控制系統項目為xx型號的一個分系統，也是該型號任務的最重要的關鍵技術。申請人負責xx衞星編隊控制系統研製，本人主要負責該項目的編隊構形初始化、構形重構、構形維持的算法設計與軟件編寫及測試。兩顆衞星於2019成功發射。

該衞星是我國首顆超低軌道xxx飛行衞星，目前負責該型號衞星的姿態與軌道控制系統研究。該系統的關鍵技術包括撓性衞星的敏捷機動和高精度軌道控制。

本人博士畢業後於2011.2-2013.5期間在新加坡一家衞星研發單位“ST Electronics (Satellite Systems) Pte Ltd”擔任衞星姿態控制工程師。主要負責衞星TeLEOS-1的姿態確定與控制算法設計與測試。TeLEOS-1是新加坡首顆自主研發的光學遙感商業衞星。TeLEOS-1於2015年12月由印度PSLV火箭成功發射。該衞星對姿態系統要求很高。一方面，為了提高成像分辨率，要求衞星具有高指向精度和高穩定度。另一方面，該衞星具備多種靈巧成像模式，包括多目標成像、拼接成像和非沿星下點軌跡成像。

Wang, Danwei, B. Wu, and E. K. Poh.Satellite Formation Flying. Springer Singapore, 2017. ^[2] 

[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, 2020, In Press.

[6]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.

[7]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.

[8] 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. In Press, 2020.DOI: 10.1109/TAES.2020.3003119

[9] 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.

[10] Hu Yabo, Geng Yunhai, Wu Baolin*, Wang Danwei, Model-Free Prescribed Performance Control for Spacecraft Attitude Tracking, IEEE Transactions on Control Systems Technology, In Press, DOI: 10.1109/TCST.2020.2968868.

[11]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

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

[13] Jinxiu Zhang, Zhigang Zhang, Baolin Wu*, Decentralized adaptive sliding mode control for beam synchronization of tethered InSAR system, Acta Astronautica 127, 57-66, 2016.

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

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

[16]Baolin Wu*, Chuang Xu, and Yingchun Zhang, Decentralized Adaptive Control for Attitude Synchronization of Multiple Spacecraft via Quantized Information Exchange, Acta Astronautica, 2020, In Press.

[17] 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

[18] 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

[19]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.

[20]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. ^[3] 

[21]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, In Press.

[22] Baolin Wu*, Guangyan Xu, Xibin Cao, Relative Dynamics and Control for Satellite Formation: Accommodating J2 Perturbation, Journal of Aerospace Engineering, 2016.

[23] 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.

[24] 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, 2011.

[25] 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. ^[4] 

[26] 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

[27] 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. ^[5] 

[28] 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.

[29] Baolin Wu*, Xibin Cao, Decentralized Control for Spacecraft Formation in Elliptic Orbits, Aircraft Engineering and Aerospace Technology, In Press.

[30] 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.

[31]Tao Yi, Yunhai Geng, and Baolin Wu*, Singularity Radius Gradient-Based Rapid Singularity-Escape Steering Law for SGCMGs, Chinese Journal of Aeronautics, In Press.

[32] 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, In Press.

[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航天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航天器姿態跟蹤控制,宇航學報 38(6), 2017, pp. 598-604.

[4] 吳寶林, 曹喜濱, 任子武, “一種長期穩定的衞星編隊隊形優化設計方法”, 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, 基於模型預測的衞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.

[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.