1991，7 获得哈尔滨工业大学自动控制专业工学学士学位

1997，1 获得哈尔滨工业大学飞行器控制、制导与仿真专业工学博士学位

1997，4－1999，5 清华大学自动化系博士后

1999，6－2001，10 哈尔滨工业大学控制科学与工程系副教授

2001，11－2003，10 日本上智大学机械工程系客座研究员JSPS Fellow

2003，1－现在 哈尔滨工业大学控制理论与制导技术研究中心教授

社会任职: 日本航空与宇宙学会会员




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学科
导航制导与控制


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研究方向
非线性控制理论及其在飞行器制导和控制中的应用


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论著成果

主要论著：

1.周荻 著，寻的导弹新型导引规律，国防工业出版社出版，2002，9

2.Zhou Di, Zhang Yong-An, Duan Guang-Ren, Multiple Model Adaptive Two-Step Filter and Motion Tracking Sliding-Mode Guidance for Missiles with Time Lag in Acceleration, Transactions of the Japan Society for Aeronautical and Space Sciences, 2004, 47(156):81-89

3.Zhou Di, Mu Chundi. Optimal Rescue Trajectories for Manned Maneuvering Unit, Transactions of the Japan Society for Aeronautical and Space Sciences, 2002, 44 (146): 200~207

4.Li, Dongmei, Zhou Di, et. al., Application of Optimal Preview Control to Terrain Following System，Chinese J. of Sys. Sci. and Elec., 2002,13(1):21-26

5.Li Dongmei, Zhou Di, Hu Zhenkun, Hu Hengzhang. Design of Optimal Preview controller for Terrain-Following Flight, Transactions of the Japan Society for Aeronautical and Space Sciences, 2001, 44 (145):142-149

6.Zhou Di, Mu Chundi, Shen Tielong. Robust Guidance Law with L2 Gain Performance, Transactions of the Japan Society for Aeronautical and Space Sciences, 2001, 44 (144): 82~88

7.Zhou Di, Mu Chundi. Motion tracking sliding-mode guidance of a homing missile with bearings only measurements, Transactions of the Japan Society for Aeronautical and Space Sciences, 2000,43 (141):130-136.

8.Zhou Di, Mu Chundi, and Xu Wenli. Adaptive Two-Step Filter with Applications to Bearings-Only Measurements Problem, AIAA Journal of Guidance, Control and Dynamics, 1999,22(5):726-728.

9.Zhou Di, Mu chundi, and Xu Wenli. Adaptive Sliding-Mode Guidance of a Homing-Missile, AIAA Journal of Guidance, Control and Dynamics , 1999,22(4):589-594.

10.Zhou Di, Mu Chundi, Ling Qiang, and Xu Wenli. Optimal Sliding-Mode Guidance of a Homing Missile, Chinese Journal of Aeronautics,1999,12(4):236-241

11.Zhou Di, Mu Chundi, and Xu Wenli, Fuzzy Adaptive Variable Structure Guidance for Space Interception. Tsinghua Science and Technology, 1999,4(4): 1610-1614


科研成果：2000年12月，国防科学技术三等奖，制导控制方法及导引规律深化研究第一名。