周荻

哈尔滨工业大学教授
哈尔滨工业大学教授，博士生导师，曾获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。兼任 日本航空与宇宙学会会员。
人物简介
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
所属学科
导航制导与控制
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
论著成果
近期主要论著
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，寻的导弹新型导引规律，国防工业出版社出版，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.