人物簡介
1991，7 獲得哈爾濱工業大學自動控制專業工學學士學位
1997，1 獲得哈爾濱工業大學飛行器控制、制導與仿真專業工學博士學位
1997，4－1999，5 清華大學自動化系博士後
1999，6－2001，10 哈爾濱工業大學控制科學與工程系副教授
2001，11－2003，10 日本上智大學機械工程系客座研究員JSPS Fellow
2003，1－現在 哈爾濱工業大學控制理論與制導技術研究中心教授
所屬學科
導航制導與控制
研究方向
非線性控制理論及其在飛行器制導和控制中的套用
論著成果
近期主要論著
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): 150-157
•Zhang G,Zhou D,Mortari D. Optimal Two-Impulse Rendezvous Using Constrained Multiple-Revolution Lambert Solutions[J]. Celestial Mechanics and Dynamical Astronomy, 2011, 110(4): 305-317
•Zhang G,Daniele M,Zhou D, Constrained Multiple-Revolution Lambert's Problem[J], AIAA Journal of Guidance, Control, and Dynamics, 2010,33(6):1779-1786
•Zhang 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: 319-336
•Zhou D, Sun S,Teo K L，Guidance Laws with Finite Time Convergence[J]，AIAA Journal of Guidance, Control and Dynamics, 2009,32(6):1838-1846
•Zhou D,Shao C-T, Dynamics and autopilot design for endoatmospheric interceptors with dual control systems[J], Aerospace Science and Technology, 2009,13(6):291-300
•Zhang 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):18-26
•Zhou 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):592-599
•Zhou 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):7-12
•Zhou 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，尋的飛彈新型導引規律，國防工業出版社出版，2002，9
•Zhou 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): 200-207
•Zhou 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): 82-88
•Zhou 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.
