| Decentralized robust adaptive control for attitude synchronization under directed communication topology B Wu, D Wang, EK Poh Journal of Guidance, Control, and Dynamics 34 (4), 1276-1282, 2011 | 140 | 2011 |
| Decentralized sliding‐mode control for attitude synchronization in spacecraft formation B Wu, D Wang, EK Poh International Journal of Robust and Nonlinear Control 23 (11), 1183-1197, 2013 | 131 | 2013 |
| Event-triggered attitude control of spacecraft B Wu, Q Shen, X Cao Advances in Space Research 61 (3), 927-934, 2018 | 114 | 2018 |
| Spacecraft attitude control with input quantization B Wu Journal of Guidance, Control, and Dynamics 39 (1), 176-181, 2016 | 90 | 2016 |
| Nonlinear optimization of low-thrust trajectory for satellite formation: Legendre pseudospectral approach B Wu, D Wang, EK Poh, G Xu Journal of Guidance, Control, and Dynamics 32 (4), 1371-1381, 2009 | 86 | 2009 |
| High precision satellite attitude tracking control via iterative learning control B Wu, D Wang, EK Poh Journal of Guidance, Control, and Dynamics 38 (3), 528-534, 2015 | 72 | 2015 |
| Rigid-body attitude stabilization with attitude and angular rate constraints Q Shen, C Yue, CH Goh, B Wu, D Wang Automatica 90, 157-163, 2018 | 70 | 2018 |
| Robust attitude tracking control for spacecraft with quantized torques B Wu, X Cao IEEE transactions on Aerospace and Electronic Systems 54 (2), 1020-1028, 2017 | 61 | 2017 |
| Model-free prescribed performance control for spacecraft attitude tracking Y Hu, Y Geng, B Wu, D Wang IEEE Transactions on Control Systems Technology 29 (1), 165-179, 2020 | 55 | 2020 |
| Neural-network-based adaptive event-triggered control for spacecraft attitude tracking W Liu, Y Geng, B Wu, D Wang IEEE transactions on neural networks and learning systems 31 (10), 4015-4024, 2019 | 51 | 2019 |
| Distributed adaptive event-triggered control for attitude synchronization of multiple spacecraft C Xu, B Wu, X Cao, Y Zhang Nonlinear Dynamics 95, 2625-2638, 2019 | 48 | 2019 |
| Rigid-body attitude tracking control under actuator faults and angular velocity constraints Q Shen, C Yue, CH Goh, B Wu, D Wang IEEE/ASME Transactions on Mechatronics 23 (3), 1338-1349, 2018 | 48 | 2018 |
| Distributed fixed-time output-feedback attitude consensus control for multiple spacecraft C Xu, B Wu, D Wang, Y Zhang IEEE Transactions on Aerospace and Electronic Systems 56 (6), 4779-4795, 2020 | 44 | 2020 |
| Shape-based analytic safe trajectory design for spacecraft equipped with low-thrust engines K Zeng, Y Geng, B Wu Aerospace Science and Technology 62, 87-97, 2017 | 41 | 2017 |
| Time-optimal reorientation for rigid satellite with reaction wheels H Zhou, D Wang, B Wu, EK Poh International journal of control 85 (10), 1452-1463, 2012 | 41 | 2012 |
| Multi-objective output-feedback control for microsatellite attitude control: An LMI approach B Wu, X Cao, Z Li Acta Astronautica 64 (11-12), 1021-1031, 2009 | 38 | 2009 |
| Satellite formation flying: relative dynamics, formation design, fuel optimal maneuvers and formation maintenance D Wang, B Wu, EK Poh Springer, 2016 | 37 | 2016 |
| Decentralized sliding-mode control for spacecraft attitude synchronization under actuator failures B Wu, D Wang, EK Poh Acta Astronautica 105 (1), 333-343, 2014 | 36 | 2014 |
| Satellite formation flying D Wang, B Wu, EKP Chung Springer Singapore) URL https://doi. org/10 1007, 978-981, 2017 | 34 | 2017 |
| Time efficient spacecraft maneuver using constrained torque distribution X Cao, C Yue, M Liu, B Wu Acta Astronautica 123, 320-329, 2016 | 33 | 2016 |
Qiang ShenShanghai Jiao Tong universityVerified email at sjtu.edu.cn
