Quaternion-based finite time control for spacecraft attitude tracking S Wu, G Radice, Y Gao, Z Sun
Acta Astronautica 69 (1-2), 48-58, 2011
160 2011 Relative motion coupled control based on dual quaternion JY Wang, HZ Liang, ZW Sun, SN Wu, SJ Zhang
Aerospace Science and Technology 25 (1), 102-113, 2013
110 2013 Sliding-mode control for staring-mode spacecraft using a disturbance observer SN Wu, XY Sun, ZW Sun, XD Wu
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2010
59 2010 Robust finite-time control for flexible spacecraft attitude maneuver S Wu, G Radice, Z Sun
Journal of Aerospace Engineering 27 (1), 185-190, 2014
49 2014 Robust S Wu, S Wen
Nonlinear Dynamics 84 (1), 405-412, 2016
46 2016 Robust attitude maneuver control of spacecraft with reaction wheel low-speed friction compensation S Wu, R Wang, G Radice, Z Wu
Aerospace Science and Technology 43, 213-218, 2015
35 2015 Gravitational orbit–attitude coupling dynamics of a large solar power satellite Y Liu, S Wu, K Zhang, Z Wu
Aerospace Science and Technology 62, 46-54, 2017
34 2017 Robust optimal sun-pointing control of a large solar power satellite S Wu, K Zhang, H Peng, Z Wu, G Radice
Acta Astronautica 127, 226-234, 2016
32 2016 Error analysis and cycle-slip detection research on satellite-borne GPS observation Y Miao, ZW Sun, SN Wu
Journal of Aerospace Engineering 24 (1), 95-101, 2011
31 2011 Active shape control of an antenna reflector using piezoelectric actuators X Song, S Tan, E Wang, S Wu, Z Wu
Journal of intelligent material systems and structures 30 (18-19), 2733-2747, 2019
30 2019 Adaptive control for spacecraft relative translation with parametric uncertainty S Wu, Z Wu, G Radice, R Wang
Aerospace Science and Technology 31 (1), 53-58, 2013
30 2013 Parametrical excitation model for rigid–flexible coupling system of solar power satellite Y Liu, S Wu, K Zhang, Z Wu
Journal of Guidance, Control, and Dynamics 40 (10), 2674-2681, 2017
28 2017 Experimental studies on model reference adaptive control with integral action employing a rotary encoder and tachometer sensors GQ Wu, SN Wu, YG Bai, L Liu
Sensors 13 (4), 4742-4759, 2013
27 2013 Multi-objective integrated robust H∞ control for attitude tracking of a flexible spacecraft S Wu, W Chu, X Ma, G Radice, Z Wu
Acta Astronautica 151, 80-87, 2018
26 2018 Active shape adjustment of large cable-mesh reflectors using novel fast model predictive control G Xun, H Peng, S Wu, Z Wu
Journal of aerospace engineering 31 (4), 04018038, 2018
24 2018 Hybrid thrusters and reaction wheels strategy for large angle rapid reorientation with high precision D Ye, Z Sun, S Wu
Acta Astronautica 77, 149-155, 2012
24 2012 Multibody dynamics and robust attitude control of a MW-level solar power satellite K Zhang, S Wu, Z Wu
Aerospace Science and Technology 111, 106575, 2021
23 2021 Robust control for spacecraft rendezvous with a noncooperative target SN Wu, WY Zhou, SJ Tan, GQ Wu
The Scientific World Journal 2013, 2013
21 2013 Distributed adaptive vibration control for solar power satellite during on-orbit assembly E Wang, S Wu, Z Wu, G Radice
Aerospace Science and Technology 94, 105378, 2019
20 2019 Gravity-gradient effects on flexible solar power satellites Y Liu, S Wu, G Radice, Z Wu
Journal of Guidance, Control, and Dynamics 41 (3), 777-782, 2018
20 2018 
Gianmarco RadiceUniversity of GlasgowEmail verificata su glasgow.ac.uk
