个人简历

工作经历
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科学与工程系教授
教育经历
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
奖项成果
2000年12月，国防科学技术三等奖(排名1)
2008年12月，国防科学技术进步三等奖(排名1)
2017年12月，黑龙江省自然科学二等奖（排名1），考虑导弹动态特性的滑模制导律设计理论及应用

研究领域

非线性控制和滤波理论
飞行器制导控制的新方法

近期论文

Shi, Xiao-Ning, Zhou, Zhi-Gang and Zhou, Di. Finite-Time Attitude Trajectory Tracking Control of Rigid Spacecraft. IEEE Transactions on Aerospace and Electronic Systems, 2017, 53(6): 2913-2923.
Zhou Chengbao, Zhou Di. Robust dynamic surface sliding mode control for attitude tracking of flexible spacecraft with an extended state observer. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2017, 231(3):533-547
Qu Pingping, Zhou Di, Sun Sheng, Observer-Based Guidance Law With Impact Angle Constraint, Journal Of Dynamic Systems Measurement and Control-Transactions of the ASME, 2017,139(11)
Shi Xiao-Ning, Zhang Yong-An, Zhou Di. Almost-global finite-time trajectory tracking control for quadrotors in the exponential coordinates. IEEE Transactions on Aerospace and Electronic Systems, 2017, 53(1): 91-100.
Sun Sheng, Zhou Di, Zhou Jingyang, Teo Kok Lay, A generalized design method for three-dimensional guidance laws, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,2017,231(1):47-60
Xu Biao，Zhou Di，Liang Zhuo，Zhou Guofeng, Robust Adaptive Sliding Sector Control and Control Allocation of a Missile with Aerodynamic Control Surfaces and Reaction Jets, Proceedings of the Institution of Mechanical Engineers, Part G- Journal of Aerospace Engineering, 2016,231(3):397-406
Zhou Di, Xu, Biao, Adaptive Dynamic Surface Guidance Law with Input Saturation Constraint and Autopilot Dynamics, Journal of Guidance Control and Dynamics , 2016,39(5): 1152-1159
Xu, Biao, Zhou Di, Sun, Sheng, Finite Time Sliding Sector Guidance Law with Acceleration Saturation Constraint, IET Control Theory and Applications, 2016,10(7):789-799
Zou Xinguang, Zhou Di, Du Runle, Adaptive Nonsingular Terminal Sliding Mode Cooperative Guidance Law in Active Defense Scenario, Proceedings of the Institution of Mechanical Engineers Part G-Journal of Aerospace Engineering,2016,230(2):307-320
Du Runle, Meng Kezi, Zhou Di, Design of Three-Dimensional Nonlinear Guidance Law with Bounded Acceleration Command, Aerospace Science and Technology, 2015,46(6):168-175
Shi Xiao-Ning, Zhang Yong-An, Zhou Di. A Geometric Approach for Quadrotor Trajectory Tracking Control [J]. International Journal of Control, 2015, 88(11):2217-2227.
Qu Pingping, Shao Chuntao, Zhou Di, Finite Time Convergence Guidance Law Accounting for Missile Autopilot, Journal Of Dynamic Systems Measurement and Control-Transactions of the ASME,2015,137(5): 051014
Di Zhou, Sheng Sun, Jing Yang Zhou, Kok Lay Teo, A Discrete Sliding-Mode Guidance Law, ASME Journal of Dynamic Systems, Measurement and Control, 2015, 137(1):024501-1-6
Sheng Sun; *Di Zhou; Wen-tao Hou, A guidance law with finite time convergence accounting for autopilot lag, Aerospace Science and Technology, 2013,25(1), pp 132-137
Di Zhou, Pingping Qu, Sheng Sun. A Guidance Law with Terminal Impact Angle Constraint Accounting for Missile Autopilot[J]. ASME Journal of Dynamic Systems, Measurement and Control, 2013, 135(5): 051009-1-10.
Pingping Qu, Di Zhou. A Dimension Reduction Observer-based Guidance Law Accounting for Dynamics of Missile Autopilot[J]. Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2013, 227(7): 1114-1121.
Zhang, Gang; Zhou, Di; Sun, Zhaowei; Cao, Xibin, Optimal periodic relative orbit and rectilinear relative orbits with eccentric reference orbits, Celestial Mechanics and Dynamical Astronomy,2013,117(2):137-148
Zhang, Gang; Zhou, Di; Sun, Zhaowei; Cao, Xibin,Optimal Two-Impulse Cotangent Rendezvous Between Coplanar Elliptical Orbits,Journal of Guidance, Control, and Dynamics, 2013,36(3): 677-685
Zhang G, Zhou D, Mortari D, Henderson T. Analytical Study of Tangent Orbit and Conditions for Its Solution Existence[J]. AIAA Journal of Guidance, Control, and Dynamics, 2012, 35(1): 186-194
Zhang G, Zhou D, Bai X. Tangent Orbital Rendezvous with the Same Direction of Terminal Velocities[J]. AIAA Journal of Guidance, Control, and Dynamics, 2012, 35(1): 335-339
日本航空与宇宙学会会员