基本信息科学研究论文专著
基本信息




工作经历
时间工作经历
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


社会任职
日本航空与宇宙学会会员


科研项目

项目名称新型非线性滤波及其在寻的制导中的应用

项目来源国家自然科学基金

开始时间2001-01-01

结束时间2003-12-01

项目经费19

担任角色负责
项目类别纵向项目
项目状态完成


项目名称动态系统同步控制方法及其在航天器姿态控制中的应用

项目来源国家自然科学基金

开始时间2007-01-01

结束时间2009-12-01

项目经费25

担任角色负责
项目类别纵向项目
项目状态完成


项目名称考虑导弹动态特性的有限时间收敛导引律

项目来源国家自然科学基金

开始时间2012-01-01

结束时间2015-12-01

项目经费58

担任角色负责
项目类别横向项目
项目状态完成


项目名称**高精度导引律研究

项目来源国防973

开始时间2006-09-01

结束时间2010-06-01

项目经费65

担任角色负责
项目类别纵向项目
项目状态完成


项目名称空间太阳能发电卫星姿态稳定及振动抑制研究

项目来源航天科技创新基金

开始时间2012-01-01

结束时间2014-12-01

项目经费10

担任角色负责
项目类别横向项目
项目状态完成


项目名称对抗强博弈机动目标过载饱和约束最优滑模制导律研究

项目来源国家自然科学基金面上项目

开始时间201801

结束时间202112

项目经费59

担任角色负责
项目类别纵向项目
项目状态进行中


项目名称末端非线性弹道智能预报技术

项目来源国防基础科研

开始时间201801

结束时间202012

项目经费180

担任角色负责
项目类别纵向项目
项目状态进行中


项目名称XX飞行器（BPV）平台设计系统

项目来源航天科技集团

开始时间201808

结束时间202008

项目经费320

担任角色负责
项目类别横向项目
项目状态进行中


项目名称XX飞行器（BPV）平台设计系统

项目来源航天科技集团

开始时间201808

结束时间202008

项目经费320

担任角色负责
项目类别横向项目
项目状态进行中


研究领域
主要研究方向:非线性控制和滤波理论

飞行器制导控制的新方法

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


论著成果
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

Zhou D, Zhang G. A Solution to Two-Point Boundary Value Problem for Power-Limited Rendezvous with Constant Thrust[J]. Acta Astronautica, 2011, 69(3-4): 150-157Zhang G, Zhou D, Mortari D. Optimal Two-Impulse Rendezvous Using Constrained Multiple-Revolution Lambert Solutions[J]. Celestial Mechanics and Dynamical Astronomy, 2011, 110(4): 305-317Zhang G, Daniele M, Zhou D, Constrained Multiple-Revolution Lambert@#%s Problem[J], AIAA Journal of Guidance, Control, and Dynamics, 2010,33(6):1779-1786Zhang Gang, and Zhou Di, A Second-Order Solution to the Two-Point Boundary Value Problem for Rendezvous in Eccentric Orbits[J], Celestial Mechanics and Dynamical Astronomy, 107(3), 2010: 319-336Zhou D, Sun S, Teo K L，Guidance Laws with Finite Time Convergence[J]，AIAA Journal of Guidance, Control and Dynamics, 2009,32(6):1838-1846Zhou D, Shao C-T, Dynamics and autopilot design for endoatmospheric interceptors with dual control systems[J], Aerospace Science and Technology, 2009,13(6):291-300Zhang Y-A, Zhou D, Sequential Multiple Model Filtering with Interrupted Measurements[J], Transactions of the Japan Society for Aeronautical and Space Sciences, 2007,50(167):18-26Zhou D, Shen T-L, Tamura K, Adaptive Nonlinear Synch. Control of Twin-Gyro Precession[J], ASME J. of Dynamic Systems, Meas., and Contr. 2006,128(3):592-599Zhou D, Shen T-L, Tamura K, Nonlinear and Adaptive Nonlinear Controllers for Attitude Stabilization and Tracking of a Spacecraft[J], Transactions of the Japan Society for Aeronautical and Space Sciences, 2005,48(159):7-12Zhou D, Zhang Y-A, Duan G-R, Multiple Model Adaptive Two-Step Filter and Motion Tracking Sliding-Mode Guidance for Missiles with Time Lag in Acceleration[J], Transactions of the Japan Society for Aeronautical and Space Sciences, 2004, 47(156):81-89周荻 著，寻的导弹新型导引规律，国防工业出版社出版，2002，9Zhou D, Mu C-D. Optimal Rescue Trajectories for Manned Maneuvering Unit[J], Transactions of the Japan Society for Aeronautical and Space Sciences, 2002, 44 (146): 200-207Zhou D, Mu C-D, Shen T-L. Robust Guidance Law with L2 Gain Performance[J], Transactions of the Japan Society for Aeronautical and Space Sciences, 2001, 44 (144): 82-88Zhou D, Mu C-D. Motion tracking sliding-mode guidance of a homing missile with bearings only measurements[J], Transactions of the Japan Society for Aeronautical and Space Sciences, 2000,43 (141):130-136.Zhou D, Mu C-D, Xu W-L. Adaptive Two-Step Filter with Applications to Bearings-Only Measurements Problem[J], AIAA Journal of Guidance, Control and Dynamics, 1999,22(5):726-728.Zhou D, Mu C-D, Xu W-L.. Adaptive Sliding-Mode Guidance of a Homing-Missile[J], AIAA Journal of Guidance, Control and Dynamics , 1999,22(4):589-594.