叶东 - 哈尔滨工业大学

个人简介

叶东，男，汉族，1985年生。教授，博士生导师，哈尔滨工业大学卫星技术研究所。近年来一直从事卫星总体、智能感知与博弈对抗、飞行器动力学与控制、航天器物理仿真等研究工作。2016年以来以第一或通讯作者在IEEE TAES、AIAA JGCD、航空学报等航天领域重要期刊发表学术论文40余篇，包括JCR I区26篇，中科院1区17篇，中科院分区TOP期刊16篇，ESI高被引1篇。航天领域SCI期刊Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 副主编。主持了国家自然科学基金青年基金、国家自然科学基金面上项目、国家重点研发计划课题等国家部委项目10余项，总计经费超2000万；作为副总师或主任设计师参研了鹊桥通导技术试验B星、“龙江二号”卫星、新技术试验卫星E星等型号任务，作为技术骨干参研了国家重点研发计划、国家自然科学基金重点项目等国家部委项目。指导多个学生科技创新项目，并获国家级竞赛一等奖3项、国家级竞赛三等奖5项，省级竞赛一等奖1项。工作经历 2021.12 至今，哈尔滨工业大学，教授 2018.01-2021.11，哈尔滨工业大学，副教授 2013.12-2017.12，哈尔滨工业大学，讲师教育经历 2003.09-2007.07，哈尔滨工业大学，航空宇航科学与技术，学士 2007.09-2009.07，哈尔滨工业大学，航空宇航科学与技术，硕士 2009.09-2013.07，哈尔滨工业大学，航空宇航科学与技术，博士 2011.10-2013.02，美国佐治亚理工，航天工程系，联合培养博士

研究领域

航天器智能博弈对抗航天器动力学与控制新概念航天器设计航天器物理仿真验证

近期论文

查看导师最新文章（温馨提示：请注意重名现象，建议点开原文通过作者单位确认）

Ye Dong, Zou An-Min, and Sun Zhaowei. Predefined-Time Predefined-Bounded Attitude Tracking Control for Rigid Spacecraft. IEEE Transactions on Aerospace and Electronic Systems. doi: 10.1109/TAES.2021.3103258. Ye Dong, Xiao Yan, Sun Zhaowei, et al. Neural Network-based Finite-time Attitude Tracking Control of Spacecraft with Angular Velocity Sensor Failures and Actuator Saturation[J]. IEEE Transactions on Industrial Electronics, 2021. Ye Dong, Shi Mingming*, Sun Zhaowei. Satellite proximate pursuit-evasion game with different thrust configurations[J]. Aerospace Science and Technology, 2020, 99: 105715. Ye Dong, Shi Mingming*, Sun Zhaowei. Satellite proximate interception vector guidance based on differential games[J]. Chinese Journal of Aeronautics, 2018, 31(6): 1352-1361. Ye Dong*, Tang Xu, Sun Zhaowei. Multiple model adaptive intercept strategy of spacecraft for an incomplete-information game. Acta Astronautica, 2021, 180:340-349 Xiao Yan, J. de Ruiter A H, Ye Dong*, Sun Zhaowei. Attitude Tracking Control for Rigid-Flexible Coupled Spacecraft with Guaranteed Performance Bounds[J]. Journal of Guidance, Control, and Dynamics, 2020, 43(2): 327-337. Ye Dong, Li You*, Xiao Bing, et al. Robust finite-time adaptive control algorithm for satellite fast attitude maneuver[J]. Journal of the Franklin Institute, 2020, 357(16): 11558-11583. Ye Dong, Xiao Yan*. Robust output feedback attitude tracking control for rigid-flexible coupling spacecraft. Journal of the Franklin Institute[J], 2018, 355(18): 9209-9223. Tang Xu, Ye Dong*, Huang L, et al. Pursuit-evasion game switching strategies for spacecraft with incomplete-information[J]. Aerospace Science and Technology, 2021: 107112. Yu Linyu, Ye Dong*, Sun Zhaowei. Finite-time resilient attitude coordination control for multiple rigid spacecraft with communication link faults[J]. Aerospace Science and Technology, 2021, 111: 106560. Zhang Zhongzheng, Ye Dong*, Xiao Bing, et al. Third‐order sliding mode fault‐tolerant control for satellites based on iterative learning observer[J]. Asian Journal of Control, 2019, 21(1): 43-51. Li You, Ye Dong*. Robust PID controller for flexible satellite attitude control under angular velocity and control torque constraint[J]. Asian Journal of Control, 2020,22(3): 1327-1344. Song Qiliang, Ye Dong*, Sun Zhaowei, Wang B. Autonomous reconfiguration of homogeneous pivoting cube modular satellite by deep reinforcement learning[J]. Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, 2021, 235(10): 1777-1786. Xiao Yan, Ye Dong*, Sun Zhaowei. Observer-based continuous finite-time attitude control for rigid–flexible coupling satellites[J]. International Journal of Control, 2019, 92(11): 2667-2680. Ye Dong, Zhang Hongzhu, Tian Yingxin, et al. Fuzzy Sliding Mode Control of Nonparallel-ground-track Imaging Satellite with High Precision[J]. International Journal of Control, Automation and Systems, 2020: 1-12. Ye Dong, Lu Wei, Mu Zhongcheng, et al. Compound control for autonomous docking to a three-axis tumbling target[J]. Transactions of the Institute of Measurement and Control, 2019, 41(4): 911-924. Ye Dong, Zhang Xiao, Wan Xucheng, et al. Finite Time Control Strategy for Satellite Attitude Maneuver Based on Hybrid Actuator[J]. Transactions of the Institute of Measurement and Control, 2018, 40(9): 2798-2806. Zhang Jianqiao, Ye Dong* , Biggs J D , et al. Finite-time relative orbit-attitude tracking control for multi-spacecraft with collision avoidance and changing network topologies[J]. Advances in Space Research, 2019, 63(3):1161-1175. Zhang Jianqiao, Ye Dong*, Sun Zhaowei, et al. Extended state observer based robust adaptive control on SE (3) for coupled spacecraft tracking maneuver with actuator saturation and misalignment[J]. Acta Astronautica, 2018, 143: 221-233. Li You, Ye Dong*, Sun Zhaowei. Time efficient sliding mode controller based on Bang-Bang logic for satellite attitude control[J]. Aerospace Science and Technology, 2018, 75: 342-352. Xiao Yan, Ye Dong*, Sun Zhaowei. Finite Time Fault-tolerant Attitude Control for Rigid-Flexible Coupling Satellites Based on Legendre Neural Network[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2018, 232(15): 2845-2857. Cheng Yu, Ye Dong*, Sun Zhaowei, et al. Spacecraft reorientation control in presence of attitude constraint considering input saturation and stochastic disturbance[J]. Acta Astronautica, 2018, 144: 61-68. 王博, 叶东*, 孙兆伟, 等.模块化可重构卫星在轨自重构的分层规划[J]. 航空学报, 2019, 40(09): 276-288. 王淳宝, 叶东*, 孙兆伟, 等.航天器末端拦截自适应博弈策略[J]. 宇航学报, 2020, 41(03): 309-318. 张众正, 叶东*, 孙兆伟. 基于迭代学习观测器的卫星姿态滑模容错控制[J]. 国防科技大学学报, 2018, 40(1): 17-23. 孔繁泽, 叶东*, 柳子然, 等. 卫星轨道递推的 GPU 集成式并行加速方法[J]. 哈尔滨工业大学学报, 2021, 53(6): 13-20.