宋申民

基本信息 科学研究 论文专著 教学与招生 新建主栏目 基本信息 名称 l 宋申民，男，汉族，山东滕州人。教授，博士生导师。现工作于哈尔滨工业大学航天学院控制理论与制导技术研究中心。 · 研究方向为：融合人工智能与经典方法的复杂系统先进控制理论与技术；先进飞行器的控制制导与仿真；智能优化方法及其在体系评估中的应用研究，飞行器组合导航技术与先进滤波方法。 · 作为项目负责人正在进行国家级重点项目、重大项目分课题、应用课题、技术加强项目、国家自然科学基金重大项目子课题、民用航天项目等十余项，其他工业横向合作课题二十余项。 · 主持完成了国家级高新技术航空航天领域项目五项、国家自然科学基金两项；主持完成航天创新基金、航天支撑基金以及航天科技集团、科工集团、航空工业集团、船舶系统工程研究院等研究院所合作项目四十余项。 · 发表科研论文一百五十余篇。其中SCI论文八十余篇，EI论文百余篇，专利五十余项，出版专著二部。 · 获部级科技进步奖一等奖一项（2023年，排名二），教育部科学技术一等奖一项，黑龙江省高等学校教学成果二等奖一项。 工作经历 名称 时间 工作经历 1996,9- 哈尔滨工业大学控制工程系控制理论与应用教研室留校工作，任讲师 1998,7- 哈尔滨工业大学控制工程系副教授 2000,10-2002,9 东京大学电气系，博士后、高级访问学者 2007,12至今 哈尔滨工业大学控制理论与制导技术研究中心，教授 2008,4至今 哈尔滨工业大学控制理论与制导技术研究中心，教授、博士生导师 教育经历 名称 1986.9―1990.7 哈尔滨工业大学计算数学与应用软件专业，获理学学士学位； 1988.9―1991.7 哈尔滨工业大学工业电气自动化专业，获工学第二学士学位； 1990.9―1993,3 哈尔滨工业大学应用数学专业，获理学硕士学位； 1993,3―1996,8 哈尔滨工业大学自动控制理论及应用专业，获工学博士学位 2000.10-2002.9 日本东京大学工学部，博士后，高级访问学者 主要学术任职 名称 国家级重点项目专家组专家 中国自动化学会平行控制与管理专业委员会委员 中国指挥与控制学会筹划与决策专业委员会委员 航空兵器学报编委 中国空间科学与技术学报编委 哈尔滨工业大学学报编委 黑龙江大学工程学报编委 中国数学学会高级会员 中国宇航学会会员 研究领域 名称 研究方向: 1. 先进飞行器控制制导协同与仿真技术 2. 飞行器组合导航与先进滤波方法 3. 智能优化理论方法及体系设计与评估 4. 融合人工智能与传统方法的复杂系统的先进控制 科研项目 项目名称 滑翔动力学与控制技术 项目来源 重点项目 开始时间 2019.01 结束时间 2022.12 项目经费 担任角色 负责 项目类别 纵向项目 项目状态 进行中 简单介绍 某类飞行器总体设计、飞行轨迹优化、导航制导与控制，攻防对抗 项目名称 装备概念体系优化设计 项目来源 纵向项目 开始时间 2020.12 结束时间 2023.12 项目经费 担任角色 负责 项目类别 纵向项目 项目状态 进行中 简单介绍 复杂环境下的体系概念设计与优化 项目名称 飞行器编队的建模与评估 项目来源 技术加强 开始时间 2020.12 结束时间 2022.6 项目经费 担任角色 负责 项目类别 纵向项目 项目状态 完成 简单介绍 项目名称 体系决策研究 项目来源 纵向项目 开始时间 2021,12 结束时间 2022.6 项目经费 担任角色 负责 项目类别 横向项目 项目状态 完成 简单介绍 项目名称 仿真建模与评估研究 项目来源 纵向项目 开始时间 2021.7 结束时间 2022.5 项目经费 担任角色 负责 项目类别 横向项目 项目状态 完成 简单介绍 飞行器的动力学、轨迹优化与控制，功放的优化与决策 项目名称 空间翻滚目标的捕获策略及组合体的快速稳定控制 项目来源 国家自然科学基金重大项目子课题 开始时间 2017.01 结束时间 2022.12 项目经费 担任角色 项目类别 项目状态 简单介绍 本项目是国家自然科学基金重大项目“空间翻滚目标捕获过程中的航天器控制理论与方法”（编号61690210）子课题 项目名称 微小卫星集群与编队控制 项目来源 国防科工局民用航天项目 开始时间 2018.11 结束时间 2022,12 项目经费 担任角色 项目类别 项目状态 简单介绍 项目名称 态势级信息下多弹协同制导攻击特性研究 项目来源 洛阳研究院 开始时间 2019.01 结束时间 2020.12 项目经费 担任角色 项目类别 项目状态 简单介绍 项目名称 弹道约束控制与仿真 项目来源 横向课题 开始时间 2017.01 结束时间 2019.12 项目经费 担任角色 项目类别 项目状态 简单介绍 项目名称 面向复杂海战场环境的精打武器研试训试验评估技术研究 项目来源 横向课题 开始时间 2019.7 结束时间 2020.12 项目经费 担任角色 项目类别 项目状态 简单介绍 项目名称 基于剩余时间控制的多约束时空协同制导技术 项目来源 航空基金重点项目 开始时间 2019.01 结束时间 2021.12 项目经费 担任角色 项目类别 项目状态 简单介绍 奖项成果 奖项名称 高精度自主辨识与交会控制技术 获奖时间 2023 完成人 张泽旭，宋申民 所获奖项 GF科技进步一等奖 简单介绍 奖项名称 控制系统的参数化设计方法及应用 获奖时间 2003 完成人 段广仁...宋申民 所获奖项 教育部自然科学奖一等奖 简单介绍 奖项名称 自动控制原理的系列化教学改革 获奖时间 2007 完成人 宋申民，王彤 所获奖项 黑龙江省高等学校教学成果二等奖 简单介绍 论著成果 名称 1. Li Jun,Song Shenmin,Prescribed time collision free trajectory tracking control for spacecraft with position-only measurements,IEEE Transactions on Aerospace and Electronic Systems,2024,February 2. Xiangzhou Gao，Shenmin Song， Hu Zhang， Zhenkun Wang，A flexible ranking-based competitive swarm optimizer for large-scale continuous multi-objective optimization ，IEEE Transactions on Evolutionary Computation 3. Honglong Kang, Pengyu Wang, Shenhui Wei, Shenmin Song. Three-Dimensional Impact-Time-Constrained Proportional Navigation Guidance Using Range-Varying Gain[J]. Aerospace Science and Technology, 2023: 108419. (SCI) 4. Kang H, Wang P, Song S. A generalized three-dimensional cooperative guidance law for various communication topologies with field-of-view constraint[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2023: 09544100231153265. (SCI) 5. Yuchen Zhang, Mengchen Ma, Xiaoyan Yang, Shenmin Song. Disturbance-observer-based fixed-time control for 6-DOF spacecraft rendezvous and docking operations under full-state constraints[J]. Acta Astronautica, 2023, 205: 225-238. 6. Zhang Y, Wu G, Yang X, Song S. Appointed-time prescribed performance control for 6-dof spacecraft rendezvous and docking operations under input saturation[J]. Aerospace Science and Technology, 2022, 128: 107744. 7. 张禹琛, 成国瑞, 宋申民. 无速度测量下的航天器安全接近位姿一体化控制[J]. 宇航学报, 2022, 43(10): 1345-1360. 8. Xiangzhou Gao, Tingrui Liu, Liguo Tan, Shenmin Song. Multioperator Search Strategy for Evolutionary Multiobjective Optimization. Swarm and Evolutionary Computation, 2022, 71:1101073. (SCI, IF=10.267, 中科院一区, 领域顶刊) 9. Gao X, Zhang H, Song S. A regularity property-driven evolutionary algorithm for multiobjective optimization[J]. Swarm and Evolutionary Computation, 2023, 78: 101258.（中科院一区top，JCR一区top，影响因子：10.267，该论文荣获2023年度国际学术“最佳研究者奖”（Best Researcher Award），奖项名称为International Research Awards on New Science Inventions ）. 10.Tingrui Liu, Liguo Tan, Xin Li, Shenmin Song. Incremental learning-inspired mating restriction strategy for Evolutionary Multiobjective Optimization[J]. Applied Soft Computing, 2022, 127: 109430. (SCI, IF=8.263, 中科院一区, 领域顶刊) 11.Tingrui Liu, Xin Li, Liguo Tan, Shenmin Song. A novel adaptive greedy strategy based on Gaussian mixture clustering for multiobjective optimization. Swarm and Evolutionary Computation, 2021, 61:100815. (SCI, IF=10.267, 中科院一区, 领域顶刊) 12.Tingrui Liu, Xin Li, Liguo Tan, Shenmin Song. An incremental-learning model-based multiobjective estimation of distribution algorithm. Information Sciences, 2021, 569(4):430-449. (SCI, IF=8.233, 中科院一区, 领域顶刊) 13.Minglei Zhuang, Liguo Tan, Kehang Li, Shenmin Song. Fixed-time formation control for spacecraft with prescribed performance guarantee under input saturation[J]. Aerospace Science and Technology, 2021, 119: 107176. (SCI检索, IF: 5.457) 14.Minglei Zhuang, Liguo Tan, Shenmin Song. Fixed-time attitude coordination control for spacecraft with external disturbance[J]. ISA Transactions, 2021, 114: 150-170. (SCI检索, IF: 5.911) 15.Minglei Zhuang, Liguo Tan, Kehang Li, Shenmin Song. Fixed-time position coordinated tracking control for spacecraft formation flying with collision avoidance[J]. Chinese Journal of Aeronautics,2021, 34(11): 182-199. (SCI检索, IF: 4.061) 16.Minglei Zhuang, Shenmin Song. Fixed-time coordinated attitude tracking control for spacecraft formation flying considering input amplitude constraint[J]. International journal of control, automation and systems, 2022, 20(7): 2129-2147. (SCI检索, IF: 2.964) 17.Minglei Zhuang, Shenmin Song, Fixed-time fault-tolerant attitude control for rigid spacecraft with torque saturation[J]. ISA transactions, 2023. (SCI检索，IF:5.911) 18.Guorui Cheng, Mengchen Ma, Liguo Tan, Shenmin Song. Gaussian Estimation for Non-linear Stochastic Uncertain Systems with Time-correlated Additive Noises and Packet Dropout Compensations [J]. IET Control Theory and Applications, 2022, 16(6): 600-614. 19.Guorui Cheng, Mengchen Ma, Liguo Tan, Shenmin Song. Event-Triggered Sequential Fusion Filter for Nonlinear Multi-Sensor Systems With Correlated Noise Based on Observation Noise Estimation [J]. IEEE Sensors Journal, 2022, 22(9): 8818-8829. 20.Guorui Cheng, Kai Zhao, Tingrui Liu, Shenmin Song. Sequential fusion state estimation algorithm for multi-sensor nonlinear systems with cross-correlated noise[C]//2022 China Automation Congress (CAC). IEEE, 2022: 1617-1621. (EI, Accepted) 21.Guanqun Wu, Liguo Tan, Xin Li, Shenmin Song. Multi-objective optimization for time-open Lambert rendezvous between non-coplanar orbits, International Journal of Aeronautical & Space Sciences, 2019, 36(1): 1-16. 22.谭立国,宋申民*,杨晓燕,霍建文. 面向小型舰船的固定翼无人机海上回收方法综述. 哈尔滨工业大学学报, 2019, 10(51):1-10. 23.Tingrui Liu, Shenmin Song, Xin Li and Liguo Tan*. Approximating Pareto Optimal Set by An Incremental Learning Model[C]//2021 IEEE Congress on Evolutionary Computation (CEC). IEEE, 2021: 169-176. 24.Meng-chen Ma, Li-guo Tan, Shen-min Song. Three-dimensional sliding mode guidance law for maneuvering target with prescribed performance and input saturation. Transactions of the Institute of Measurement and Control, 2020, 43(5): 1176-1190. (SCI) 25.Meng-chen Ma, Kai Zhao, Shen-min Song. Adaptive sliding mode guidance law with prescribed performance for intercepting maneuvering target, International Journal of Innovative Computing, Information and Control, 2019, 16(2): 631-648. (SCI) 26.Meng-chen Ma, Shen-min Song. Three-dimensional prescribed performance cooperative guidance law with spatial constraint for intercepting manoeuvring targets[J]. International Journal of Control, 2023, 96(6): 1424-1435. (SCI) 27.Mengchen Ma, Liguo Tan, Shenmin Song. Three-dimensional Prescribed Performance Sliding Mode Guidance law for Intercepting Maneuvering Target. Part G: Journal of Aerospace Engineering, 2022, 236(9): 1836-1850. 28.Xiaoyan Yang, Yuchen Zhang, Shenmin Song. Three-dimensional field-of-view-constrained guidance law against maneuvering target with intercept angle control [J]. Aerospace Science and Technology. 142 (2023). 29.Xiao-yan Yang, Yu-chen Zhang, Shen-min Song. Three-dimensional nonsingular impact angle guidance strategy with physical constraints[J]. ISA transactions, 2022, 131: 476-488. 30.Xiaoyan Yang, Yuchen Zhang, Shenmin Song. Two-Stage Cooperative Guidance Strategy with Impact-Angle and Field-of-View Constraints[J]. Journal of Guidance, Control, and Dynamics, 2023, 46(3): 590-599. 31.Xiaoyan Yang, Shenmin Song. Three-dimensional consensus algorithm for nonsingular distributed cooperative guidance strategy[J]. Aerospace Science and Technology, 2021, 118: 1270-9638. 32.Guanqun Wu, Shenmin Song, Antisaturation attitude and orbit-coupled control for spacecraft final safe approach based on fast nonsingular terminal sliding mode[J]. Journal of Aerospace Engineering, 2019, 32(2): 04019002. (SCI) 33.Wu Guanqun, Song Shenming, Sun Jingguang. Finite-time antisaturation control for spacecraft rendezvous and docking with safe constraint[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019, 233(6): 2170-2184. (SCI) 34.Wu Guanqun, Song S, Sun J. Finite-time dynamic surface anti-saturation control for spacecraft terminal approach considering safety. Journal of Spacecraft and Rockets, 2018, 55(6):1430-1443. (SCI) 35.Wu Guanqun, Song Shenming, Sun Jingguang. Adaptive dynamic surface control for spacecraft terminal safe approach with input saturation based on tracking differentiator[J]. International Journal of Control, Automation and Systems, 2018, 16: 1129-1141. (SCI，WOS:000428905600003) 36.Kai Zhao, Liguo Tan, Shenmin Song. Fusion estimation for nonlinear multi-sensor networked systems with packet loss compensation and correlated noises. Sensor Review, 2019, 39(5):682-696. 37.Kai Zhao, Liguo Tan, Shenmin Song. Gaussian filter for nonlinear networked systems with synchronously correlated noises and one-step randomly delayed measurements and multiple packet dropouts. IEEE Sensors Journal, 2019, 19(20):9271-9281.（SCI, IF=4.325, 中科院二区, 通讯作者） 38.Kai Zhao, Peng Li, Shen-Min Song，Gaussian filter for nonlinear stochastic uncertain systems with correlated noises, IEEE Sensors Journal. 2018,18(23):9584-9594. (SCI) 39.Kai Zhao, Shen-Min Song，Alternative framework of the Gaussian filter for non-linear systems with randomly delayed measurements and correlated noises，IET Science Measurement & Technology. 2017,12(2):161-168. (SCI，WOS:000427630000002) 40.Li Xue-Hui, Zhu Zhi-Bin, Song Shen-Min. Non-cooperative Rendezvous and Docking using artificial potentials and sliding mode control, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2019,233(4):1171-1184. (SCI) 41.Li Xue-Hui, Song Shen-Min. Robust finite-time tracking control for Euler-Lagrange systems with obstacle avoidance. Nonlinear Dynamics. 2018,93(2):443-451. (SCI) 42.Haitao Chen, Shenmin Song and Xuehui Li. Robust spacecraft attitude tracking control with integral terminal sliding mode surface considering input saturation. Transactions of the Institute of Measurement and Control, 2019, 41(2):405-416. (SCI) 43.Hai-Tao Chen, Shen-Min Song and Zhi-Bin Zhu. Robust Finite-time Attitude Tracking Control of Rigid Spacecraft Under Actuator Saturation. International Journal of Control, Automation and Systems. 2018,16(1):1-15. (SCI) 44.Haitao Chen, Shenmin Song. Robust chattering-free finite time attitude tracking control with input saturation[J]. Journal of Systems Science and Complexity, 2019, 32: 1597-1629. (SCI) 45.Xin Li, Hu Zhang, Shenmin Song, A Self-adaptive Mating Restriction Strategy based on Survival Length for Multiobjective Optimization, Swarm and Evolutionary Computation, 2018, 43(1): 31-49. (SCI收录号：000452933500002, JCRQ1, 中科院2区, IF=3.818) 46.Xin Li, Hu Zhang, Shenmin Song, MOEA/D with the online agglomerative clustering based self-adaptive mating restriction strategy[J]. Neurocomputing, 2019, 339: 77-93.（JCRQ1, 中科院2区, IF=3.241） 47.Xin Li, Shenmin Song, Hu Zhang, Evolutionary multiobjective optimization with clustering-based self-adaptive mating restriction strategy[J]. Soft Computing, 2019, 23: 3303-3325. (JCRQ2, 中科院3区, IF=2.367) 48.Xin Li, Hu Zhang, Shenmin Song, A decomposition based multiobjective evolutionary algorithm with self-adaptive mating restriction strategy[J]. International Journal of Machine Learning and Cybernetics, 2019, 10: 3017-3030.（JCRQ2, 中科院3区, IF=2.692） 49.Chen Zhenyu, Liu Yang, Fu Zhenxian, Song Shenmin and Tan Jiubin. Calibration of the Hall Measurement System for a 6-DOF Precision Stage Using Self-Adaptive Hybrid TLBO. Sensors, 2016, 16(6):872. (SCI, WOS:000378756500120) 50.Sun Jing-guang, Song Shen-min, Chen Hai-tao and Li Xue-Hui. Finite-time tracking control of hypersonic aircrafts with input saturation[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2018, 232(7): 1373-1389. (SCI, WOS:000433092700015) 51.Sun Jing-guang, Song Shen-min, Chen Hai-tao and Wu Guan-qun. Fast Terminal Sliding Mode Tracking Control of Hypersonic Vehicles Based on non-homogeneous Disturbance Observer. International Journal of Control, Automation, and Systems. 2017,15(6):2646-2659. (SCI, WOS:000417737300020) 52.Sun Jing-guang, Song Shen-min and Wu Guan-qun. Tracking control of hypersonic vehicle considering input constraint. Journal of Aerospace Engineering. 2017,30(6):1073-1085. (SCI, WOS:000416762600011) 53.Sun Jing-guang, Song Shen-min and Wu Guan-qun. Fault-tolerant track control of hypersonic vehicle based on fast terminal sliding mode[J]. Journal of spacecraft and rockets, 2017, 54(6): 1304-1316. (SCI, WOS:000415993200013) 54.Sun Jing-Guang, Xu Sheng-Li, Song Shen-Min and Dong Xi-Jun. Finite time tracking control of hypersonic vehicles with input saturation. Aerospace science and technology. 2017,71:272-284. (SCI, WOS:000433092700015) 55.Dong Jipeng, Sun Jingguang, Guo Yong and Song Shenmin. Guidance laws against towed decoy based on adaptive back-stepping sliding mode and anti-saturation methods[J]. International Journal of Control, Automation and Systems, 2018, 16: 1724-1735. (SCI) 56.Xiao-Hang Wu, Shen-Min Song, Consistency monitoring for spacecraft attitude estimators[J]. Journal of Aerospace Engineering, 2019, 32(2): 04018145. (SCI，Accepted) 57.Xiao-Hang Wu, Shen-Min Song, Robust information unscented particle filter based on M‐estimate[J]. IET Signal Processing, 2019, 13(1): 14-20. (SCI，Accepted) 58.Xiao-Hang Wu, Shen-Min Song, Covariance intersection‐based fusion algorithm for asynchronous multirate multisensor system with cross‐correlation[J]. IET Science, Measurement & Technology, 2017, 11(7): 878-885. (SCI，WOS:000413156600008) 59.Si Yu-jie, Song Shen-min. Continuous Reaching Law Based Three-dimensional Finite-time Guidance Law against Maneuvering Targets. Transactions of the Institute of Measurement and Control. 2019,41(2):321-339. (SCI，Accepted) 60.Si Yujie, Song Shenmin, Adaptive Reaching Law Based Three-dimensional Finite-time Guidance Law against Maneuvering Targets with Input Saturation, Aerospace Science and Technology. 2017,70(6):2022-2035. (SCI，WOS:000414620400017 ) 61.Si Yujie, Song Shenmin, Three-dimensional adaptive finite-time guidance law for intercepting maneuvering targets, Chinese Journal of Aeronautics. 2017,30(6):1023-1034. (SCI，WOS:000417060500017) 62.Sun Jing-guang, Song Shen-min, Wu Guanqun. Adaptive anti-saturation fault-tolerant control of hypersonic vehicle with actuator faults. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019,233(6):2066-2083. 63.Song Junhong, Song Shenmin, Three-dimensional guidance law based on adaptive integral sliding mode control, Chinese Journal of Aeronautics, 2016, 29(1): 202-214. (SCI, WOS:000373719600016) 64.Song Junhong, Song Shenmin, Zhou Huibo, Adaptive nonsingular fast terminal sliding mode guidance law with impact angle constraints, International Journal of Control, Automation and Systems, 2016, 14(1): 99-114. (SCI, WOS:000369704900012) 65.Junhong Song, Shenmin Song, Di Zhang, Shengli Xu. Three-dimensional cooperative guidance law for multiple missiles with finite-time convergence, Aerospace Science and Technology. 2017,67:193-205. (SCI, WOS:000405053600020) 66.Guo Yong, Song Shen-min. Adaptive finite-time backstepping control for attitude tracking of spacecraft based on rotation matrix. Chinese Journal of Aeronautics, 2014,27(2): 375–382. (SCI, WOS:000334848500020) 67.Guo Yong, Song Shen-min, Deng Li-wei. Finite-time Coordination Control for Formation Flying Spacecraft. Journal of Systems Engineering and Electronics, 2014, 25(5): 859–867. (SCI, WOS:000344444900018) 68.Guo Yong, Song Shen-min, Li Xue-Hui. Terminal sliding mode control for attitude tracking of spacecraft based on rotation matrix[J]. Mathematical Problems in Engineering, 2015, 2015. (SCI, WOS:000352426600001) 69.Guo Yong, Song Shen-min, Li Xue-Hui. Quaternion-based finite time control for attitude tracking of spacecraft without unwinding. International Journal of Control, Automation, and Systems, 2015, 13(6):1351–1359. (SCI, WOS:000365378800005) 70.Guo Yong, Song Shen-min, Yan Zhibin. Finite-time coordination control for formation flying spacecraft without unwinding. Proceedings of the Institution of Mechanical Engineers Part G- Journal of aerospace engineering, 2016, 230(1):172–188. (SCI, WOS:000367401400013) 71.Guo Yong, Song Shen-min, Li Xue-Hui. Finite-time output feedback attitude coordination control for formation flying spacecraft without unwinding. Acta Astronautica, 2016, 122:159–174. (SCI, WOS:000374076000014) 72.Guo Yong, Song Shen-min, Li Xue-Hui, Li Peng. Terminal sliding mode control for the attitude tracking of the spacecraft under input saturation. Journal of Aerospace Engineering. 2017,30(3):256-263. (SCI, WOS:000399890600020) 73.Guo Yong, Song Shen-min, Li Xue-Hui. Backstepping sliding mode control for formation flying spacecraft. Aircraft Engineering and Aerospace Technology. 2018,90(1):56-64.(SCI, WOS:000424215400007) 74.Guo Yong, Song Shen-min, Li Xue-Hui, Zhu Zhibin. Finite-time output feedback control for the attitude of the spacecraft without unwinding. Proceedings of the Institution of Mechanical Engineers Part G- Journal of aerospace engineering. 2017,235(2):158-165. ( SCI, WOS:000374076000014) 75.Guo Y, Guo J, Song S. Backstepping control for attitude tracking of the spacecraft under input saturation[J]. Acta Astronautica, 2017,138(2):318-325. (SCI, WOS:000408290900030) 76. Yong Guo, Bing Huang, Shenmin Song, Robust Saturated Finite-Time Attitude Control for Spacecraft Using Integral Sliding Mode, Journal of Guidance, Control and Dynamics. 2018,42(2): 440-446. 77.Zhang Baoqun, Song Shenmin. Robust Attitude Coordination Control of Formation Flying Spacecraft under Control Input Saturation[J]. Internation Journal of Innovative Computing, Information and Control, 2011, 7(7): 4223–4235. (SCI, WOS:000292626900011) 78.Zhang Baoqun, Song Shenmin, Chen X L. Decentralized robust coordinated control for formation flying spacecraft with coupled attitude and translational dynamics[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2013, 227(5): 798-815. (SCI, WOS:000318575900005) 79.Zhang Baoqun, Song Shenmin. Decentralized Coordinated Control for Multiple Spacecraft Formation Maneuvers [J]. Acta Astronautica, 2012, 74(5–6), 79–97.( SCI, WOS:000301897800007) 80.Zheng Zhong, Song Shenmin. Autonomous attitude coordinated control for spacecraft formation with input constraint, model uncertainties, and external disturbances[J]. Chinese Journal of Aeronautics, 2014, 27(3): 602-612. (SCI, WOS:000340844900016) 81.Zheng Zhong, Song Shenmin. Cooperative attitude tracking control for multiple spacecraft using vector measurements[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2015, 229(13): 2375-2388. (SCI, WOS:000363206800003). 82.Hu Zhang, Xiujie Zhang, Xiao-Zhi Gao, Shenmin Song. Self-organizing multiobjective optimization based on decomposition with neighborhood ensemble[J]. Neurocomputing, 2016, 173: 1868–1884. (SCI, WOS:000366879800139). 83.Hu Zhang, Aimin Zhou, Shenmin Song. A self-organizing multiobjective evolutionary algorithm[J]. IEEE Transactions on Evolutionary Computation, 2016, 20(5): 792-806. (SCI, WOS:000385241600010) 84.Hu Zhang, Xiujie Zhang, Shenmin Song, Xiao-Zhi Gao. An affinity propagation-based multiobjective evolutionary algorithm for selecting optimal aiming points of missiles[J]. Soft Computing, 2017, 21: 3013-3031. (SCI, WOS:000401696600016) 85.Hu Zhang, Shenming Song, Aimin Zhou. A multiobjective cellular genetic algorithm based on 3D structure and cosine crowding measurement, International Journal of Machine Learning & Cybernetics, 2015 ,6(3):487-500. （SCI, WOS:000354391500014）. 86.Yu Han, Zhang Xiujie, Lingyu L, Liu Lingyu, Wang Shuo, Song Shenmin. Relative dynamics estimation of non-cooperative spacecraft with unknown orbit elements and inertial tensor[J]. Chinese Journal of Aeronautics, 2016, 29(2): 479-491. ( SCI, WOS:000375861300018) 87.Yu Han, Song Shenmin, Wang Shuo. Alternative framework of the Gaussian filter for non‐linear systems with synchronously correlated noises[J]. IET Science, Measurement & Technology, 2016, 10(4): 306-315. （SCI, WOS:000380258000008）. 88.Zhuibo, Song Shenmin, Song Junhong. Design of Sliding Mode Guidance Law with Dynamic Delay and Impact Angle Constraint[J]. International Journal of Control, Automation and Systems, 2017,15(1):239-247. (SCI, WOS: 000393707600026). 89.Shen-min Song, Zhuo-yi Song, Xing-lin Chen, Guang-ren Duan. Adaptive wavelet neural network friction compensation of mechanical systems[C]//Advances in Neural Networks-ISNN 2006: Third International Symposium on Neural Networks, Chengdu, China, May 28-June 1, 2006, Proceedings, Part II 3. Springer Berlin Heidelberg, 2006: 1131-1139. (IDS:BET84; WOS:000239483000166) 90.Zhen-qiang Qi, Shenmin Song, Zhao-hua Yang, Guang-da Hu, Fu-en Zhang. A novel immune feedback control algorithm and its applications[C]//Genetic and Evolutionary Computation–GECCO 2004: Genetic and Evolutionary Computation Conference, Seattle, WA, USA, June 26-30, 2004. Proceedings, Part I. Springer Berlin Heidelberg, 2004: 318-320. (IDS 号: BBE15, WOS:000225101200033 ) 91.Zhigang Yu, Shenmin Song, Guangren Duan, Run Pei. Robust adaptive neural networks with an online learning technique for robot control[C]//Advances in Neural Networks-ISNN 2006: Third International Symposium on Neural Networks, Chengdu, China, May 28-June 1, 2006, Proceedings, Part II 3. Springer Berlin Heidelberg, 2006: 1153-1159. (IDS 号: BBE84, WOS: 000239483000169 ) 92.Yanming Fu, Guangren Duan, Shenmin Song. Design of unknown input observer for linear time-delay systems[J]. International Journal of Control, Automation, and Systems. 2004, 2(4): 530-535.(IDS 号: 885MX, WOS: 000226162500013) 93.Chen H, Li X, Song S. Smooth adaptive finite time attitude tracking control of rigid spacecraft[J]. International Journal of Innovative Computing Information & Control Ijicic, 2017, 13(3):905-919. 94.于浛, 宋申民. 考虑随机量测时滞和同步相关噪声的改进高斯滤波算法. 控制理论与应用. 2016.2，33（2）：133-145. 95.于浛，宋申民，交互式容积卡尔曼滤波及其应用. 控制与决策.2015,30（9）:1660-1666. 96.于浛，魏喜庆，宋申民，基于自适应容积卡尔曼滤波的非合作航天器相对运动估计. 航空学报.2014,35（8）：2251-2260. 97.Yu Han, Song Shenmin, Algorithm of Binocular Vision Measurement for Non-cooperative Spacecraft Based on Model. Journal of Computational Information System.2014,10（4）：1717-1729. 98.宋申民, 郭永, 李学辉. 航天器姿态跟踪有限时间饱和控制. 控制与决策, 2015, 30(11): 2004-2008. 99.郭永、宋申民、李学辉. 非合作交会对接的姿态和轨道耦合控制. 控制理论与应用.2016,33(5):638-644. 100. Song Junhong, Song Shenmin. Design of Second-Order Sliding Mode Guidance Law Based on the Nonhomogeneous Disturbance Observer. International Journal of Innovative Computing, Information and Control.2015,11（3）:787-802. 101. Huibo Zhou, Shenmin Song，Design of second-order sliding mode guidance law based on the nonhomogeneous disturbance observer[J]. Journal of Control Science and Engineering, 2014, 2014: 19-19. 102. Liwei Deng, Shenmin Song. Stabilization of fractional order hyperchaotic systems with uncertainties via output feedback sliding mode control[J]. Journal of Harbin Institute Technology, 2015. (New Series). (EI). 103. 邓立为, 宋申民. 基于输出反馈滑模的分数阶超混沌系统同步控制[J]. 自动化学报. 2014, 40(11):2420-2427. 104. 邓立为，宋申民. 基于分数阶滑模的挠性航天器姿态鲁棒跟踪控制. 航空学报， 2013,34(8):1915-1923. 105. 宋申民，郑重，控制受限的编队航天器鲁棒自适应控制，宇航学报，2014,35(12):1422-1429. 106. 郑重，宋申民. 基于旋转矩阵描述的航天器无角速度测量姿态跟踪无源控制. 控制与决策，2014，29(9)：1628–1632. 107. 郑重，宋申民. 考虑避免碰撞的编队卫星自适应协同控制. 航空学报，2013, 34(8): 1934-1943. 108. 郑重，宋申民，张保群. 考虑姿态禁忌约束的航天器安全姿态跟踪控制. 系统工程与电子技术, 2013,35(3):574-579. 109. 魏喜庆，宋申民， 基于改进容积卡尔曼滤波的奇异避免姿态估计，航空学报,2013, 34(3):610-619. 110. 魏喜庆，宋申民 ，基于四元数容积卡尔曼滤波的卫星姿态估计，宇航学报,2013, 34(2):193-200. 111. 魏喜庆，宋申民 ，无模型容积卡尔曼滤波及其应用，控制与决策,2013, 28(5):769-773. 112. 魏喜庆，宋申民 ，交会对接气浮仿真平台视觉辅助姿态确定，中国空间科学技术, 2011, 10(5):41-47. 113. 魏喜庆，宋申民, ，张保群. 基于无模型无迹粒子滤波的编队卫星相对运动估计. 系统工程与电子技术. 2012, 34(6):1215-1219. 114. 张保群，宋申民，陈兴林. 带时延和拓扑切换的编队卫星鲁棒协同控制.宇航学报. 2012, 33(7)：910–919. 115. 张保群，宋申民，陈兴林．编队卫星分布式鲁棒饱和姿态协同控制．航空学报.2011，32（9）：1644-1655 116. 张保群，宋申民，陈兴林. 输入受限的编队卫星分布式姿态协同控制.中国空间科学技术，2011，31(1):16-24. 117. 张保群，宋申民，陈兴林. 考虑控制饱和的编队飞行卫星姿态协同控制. 宇航学报，2011,32(5):1160-1169 118. 张保群，宋申民，陈兴林. 编队飞行挠性航天器的输出反馈姿态协同控制. 系统工程与电子技术，2011，33（7）, 1595-1602 119. 宋申民，张保群，陈兴林. 空间绕飞任务中航天器姿态跟踪的鲁棒控制. 系统工程与电子技术. 2011, 33(1): 120-126. 120. 于志刚，宋申民 机械臂鲁棒自适应运动控制，控制理论与应用，2011，28（7）：1021-1024. 121. 宋申民，张大伟，非合作自主交会对接的动态障碍物躲避制导[J]. 中国空间科学技术, 2010 (6): 39-48. 122. Dawei Zhang, Shenmin Song，Safe guidance for autonomous rendezvous and docking with a non-cooperative target[C]//AIAA guidance, navigation, and control conference. 2010: 7592. 123. 张大伟，宋申民，非合作目标自主交会对接的椭圆蔓叶线势函数制导，宇航学报，2010，31（10）：2259-2268 124. 宋申民，吕建华. 基于Hamilton-Jacobi方程的编队飞行控制 航空学报，2008，29（2）：416-423 EI: 081611206945 125. 陈宝文 宋申民 陈兴林 基于混合算法的带时间窗车辆路径问题 控制理论与应用2007，24（5）：807-810 EI: 074910962556 126. 宋申民 于志刚 段广仁 BTT导弹自适应神经网络控制 宇航学报 2007, 28（5）:1224-1230 EI: 081211161712 127. 宋申民，宋卓异，陈兴林，段广仁. 卫星光通信粗瞄系统非线性摩擦的神经网络补偿 , 航空学报，2007, 28（2）：358-364 EI: 072310642943 128. 宋申民，张克，张炳通，陈兴林. 航天器壳体压力自动加载系统的研究 宇航学报，2005，26（4）：499-504. 运动稳定性与航天控制，宋申民著，科学出版社，2014 名称 本书清晰深入地阐述了运动稳定性的基本理论和近代发展的成果，总结了作者在航天控制研究实践中的成果。 全书主要包括：李雅普诺夫稳定性概念与主要理论和扩展；李雅普诺夫稳定性近代发展的结果，如扰动系统的稳定性与有界性、有限时间稳定性、切换系统的稳定性等；系统的输入输出特性、无源性与耗散性，尤其是与李雅普诺夫稳定性的关系；重点介绍了基于李雅普诺夫的非线性控制系统设计：反步法与滑模控制，特别是滑模控制的最新发展，如终端滑模与分数阶滑模控制等；最后一部分是稳定性理论在航天控制中的应用，如航天器的姿态控制与姿态协同控制、航天器的相对轨道机动控制与姿轨耦合控制等。附录中总结了刚体的姿态运动学与动力学模型。 本书针对控制科学与工程以及宇航科学与技术两个主要学科精心选取了稳定性的基本理论和近代稳定性理论的部分成果，并介绍了作者在航天控制中的主要研究结果。 招生信息 名称 硕士招生： 每年计划招收硕士研究生3名，主要开展基于视觉的组合导航与协同探测、先进飞行器协同制导、飞行控制等方向的研究。 博士招生： 每年计划招收博士2-4名，主要开展飞行器的协同制导与控制、高超声速飞行器弹道协同规划、组合导航与飞行控制、非合作航天器的空间博弈决策与控制等方向研究。 讲授课程 名称 稳定性理论及应用（研究生课，在讲授） 智能优化原理与算法（研究生课，在讲授） 导弹防御系统智能攻防数字仿真与推演（本科生创新研修课，在讲授） 线性系统理论（研究生课） 矩阵分析（研究生课） 现代控制理论（研究生课） 智能控制（研究生课） 自动控制原理（自动化专业本科课）