Xianghua Wang
Xianghua Wang
Shandong University of Science and Technology
確認したメール アドレス: sdust.edu.cn
タイトル引用先
Partial integrated missile guidance and control with finite time convergence
X Wang, J Wang
Journal of Guidance, Control, and Dynamics 36 (5), 1399-1409, 2013
672013
Partial integrated guidance and control for missiles with three-dimensional impact angle constraints
X Wang, J Wang
Journal of Guidance, Control, and Dynamics 37 (2), 644-657, 2014
482014
Partial integrated guidance and control with impact angle constraints
X Wang, J Wang
Journal of Guidance, Control, and Dynamics 38 (5), 925-936, 2014
372014
A novel sliding mode observer for state and fault estimation in systems not satisfying matching and minimum phase conditions
X Wang, CP Tan, D Zhou
Automatica 79, 290-295, 2017
282017
Sparse array quiescent beamformer design combining adaptive and deterministic constraints
X Wang, M Amin, X Wang, X Cao
IEEE Transactions on Antennas and Propagation 65 (11), 5808-5818, 2017
162017
Robust tracking control for an air-breathing hypersonic vehicle with input constraints
G Gao, J Wang, X Wang
International Journal of Systems Science 45 (12), 2466-2479, 2014
152014
State and unknown input estimation for a class of infinitely unobservable descriptor systems using two observers in cascade
JHT Ooi, CP Tan, WS Chua, X Wang
Journal of the Franklin Institute 354 (18), 8374-8397, 2017
142017
Adaptive fault‐tolerant control for feedback linearizable systems with an aircraft application
G Gao, J Wang, X Wang
International Journal of Robust and Nonlinear Control 25 (9), 1301-1326, 2015
142015
Partial integrated missile guidance and control with state observer
X Wang, J Wang, G Gao
Nonlinear Dynamics 79 (4), 2497-2514, 2015
122015
Three-dimensional impact angle constrained distributed guidance law design for cooperative attacks
X Wang, X Lu
ISA transactions 73, 79-90, 2018
112018
Prescribed-performance fault-tolerant control for feedback linearisable systems with an aircraft application
G Gao, J Wang, X Wang
International Journal of Control 90 (5), 932-949, 2017
52017
Partial integrated guidance and control with input constraints and impact angle
X Wang, J Wang
AIAA guidance, navigation, and control conference, 1473, 2014
42014
3-D impact angle constrained distributed cooperative guidance for maneuvering targets without angular-rate measurements
XH Wang, CP Tan
Control Engineering Practice 78, 142-159, 2018
32018
Robust sparse array design for adaptive beamforming against DOA mismatch
X Wang, M Amin, X Wang
Signal Processing 146, 41-49, 2018
32018
Distributed cooperative controller design considering guidance loop and impact angle
XH Wang, CP Tan
Journal of the Franklin Institute 355 (15), 6927-6946, 2018
22018
Partial integrated missile guidance and control with input constraints
X Wang, J Wang
Proceedings of the 32nd Chinese Control Conference, 5443-5448, 2013
22013
Fault-Tolerant Attitude Control for Rigid Spacecraft Without Angular Velocity Measurements
X Wang, CP Tan, F Wu, J Wang
IEEE Transactions on Cybernetics, 2019
12019
Autopilot and guidance law design considering impact angle and time
X Wang, CP Tan, D Zhou
IET Control Theory & Applications 12 (2), 221-232, 2017
12017
Partial integrated guidance and control for missiles considering actuator fault and saturation
X Wang, X Lu
2017 29th Chinese Control And Decision Conference (CCDC), 5097-5102, 2017
12017
Partial integrated missile guidance and control with output feedback
X Wang, J Wang, G Gao
Proceedings of the 33rd Chinese Control Conference, 713-718, 2014
12014
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