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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): 150-157
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.
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