| 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 | 93 | 2013 |
| 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 | 84 | 2017 |
| 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 | 72 | 2014 |
| Three-dimensional impact angle constrained distributed guidance law design for cooperative attacks X Wang, X Lu ISA transactions 73, 79-90, 2018 | 58 | 2018 |
| Partial integrated guidance and control with impact angle constraints X Wang, J Wang Journal of Guidance, Control, and Dynamics 38 (5), 925-936, 2015 | 56 | 2015 |
| Fault-tolerant attitude control for rigid spacecraft without angular velocity measurements X Wang, CP Tan, F Wu, J Wang IEEE transactions on cybernetics 51 (3), 1216-1229, 2019 | 48 | 2019 |
| 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 | 42 | 2017 |
| 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 | 26 | 2018 |
| Kalman filtering for delayed singular systems with multiplicative noise X Lu, L Wang, H Wang, X Wang IEEE/CAA Journal of Automatica Sinica 3 (1), 51-58, 2016 | 26 | 2016 |
| Partial integrated missile guidance and control with state observer X Wang, J Wang, G Gao Nonlinear Dynamics 79, 2497-2514, 2015 | 22 | 2015 |
| 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 | 19 | 2017 |
| 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 | 19 | 2015 |
| 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 | 18 | 2014 |
| Fault‐tolerant spacecraft attitude control under actuator saturation and without angular velocity X Wang, CP Tan International Journal of Robust and Nonlinear Control 29 (18), 6483-6506, 2019 | 16 | 2019 |
| Robust sparse array design for adaptive beamforming against DOA mismatch X Wang, M Amin, X Wang Signal Processing 146, 41-49, 2018 | 16 | 2018 |
| Distributed cooperative controller design considering guidance loop and impact angle XH Wang, CP Tan Journal of the Franklin Institute 355 (15), 6927-6946, 2018 | 14 | 2018 |
| Dynamic output feedback fault tolerant control for unmanned underwater vehicles X Wang, CP Tan IEEE Transactions on Vehicular Technology 69 (4), 3693-3702, 2019 | 13 | 2019 |
| 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 | 12 | 2017 |
| Observer-based PIGC for missiles with impact angle constraint X Wang, CP Tan, D Zhou IEEE Transactions on Aerospace and Electronic Systems 55 (5), 2226-2240, 2018 | 10 | 2018 |
| Integrated missile guidance and control using adaptive sliding mode approach W Xianghua, W Jinzhi Proceedings of the 31st Chinese Control Conference, 4611-4616, 2012 | 6 | 2012 |
Tan Chee PinProfessor, School of Engineering, Monash University MalaysiaVerified email at monash.edu
