| Dual-quaternion-based adaptive motion tracking of spacecraft with reduced control effort H Gui, G Vukovich Nonlinear Dynamics 83, 597-614, 2016 | 98 | 2016 |
| Adaptive fault‐tolerant spacecraft attitude control using a novel integral terminal sliding mode H Gui, G Vukovich International Journal of Robust and Nonlinear Control 27 (16), 3174-3196, 2017 | 89 | 2017 |
| Global finite-time attitude consensus of leader-following spacecraft systems based on distributed observers H Gui, AHJ de Ruiter Automatica 91, 225-232, 2018 | 81 | 2018 |
| Simple finite-time attitude stabilization laws for rigid spacecraft with bounded inputs H Gui, L Jin, S Xu Aerospace Science and Technology 42, 176-186, 2015 | 73 | 2015 |
| Attitude maneuver control of a two-wheeled spacecraft with bounded wheel speeds H Gui, L Jin, S Xu Acta Astronautica 88, 98-107, 2013 | 64 | 2013 |
| Distributed almost global finite-time attitude consensus of multiple spacecraft without velocity measurements H Gui, G Vukovich Aerospace Science and Technology 75, 284-296, 2018 | 59 | 2018 |
| Finite‐time angular velocity observers for rigid‐body attitude tracking with bounded inputs H Gui, G Vukovich International Journal of Robust and Nonlinear Control 27 (1), 15-38, 2017 | 59 | 2017 |
| Adaptive fault-tolerant spacecraft pose tracking with control allocation H Gui, AHJ de Ruiter IEEE Transactions on Control Systems Technology 27 (2), 479-494, 2017 | 53 | 2017 |
| Global finite-time attitude tracking via quaternion feedback H Gui, G Vukovich Systems & Control Letters 97, 176-183, 2016 | 53 | 2016 |
| Adaptive integral sliding mode control for spacecraft attitude tracking with actuator uncertainty H Gui, G Vukovich Journal of the Franklin Institute 352 (12), 5832-5852, 2015 | 52 | 2015 |
| Finite-time output-feedback position and attitude tracking of a rigid body H Gui, G Vukovich Automatica 74, 270-278, 2016 | 50 | 2016 |
| Control of asteroid-hovering spacecraft with disturbance rejection using position-only measurements H Gui, AHJ Ruiter Journal of Guidance, Control, and Dynamics 40 (10), 2401-2416, 2017 | 45 | 2017 |
| Robust adaptive tracking of rigid-body motion with applications to asteroid proximity operations G Vukovich, H Gui IEEE Transactions on Aerospace and Electronic Systems 53 (1), 419-430, 2017 | 42 | 2017 |
| Quaternion invariant extended Kalman filtering for spacecraft attitude estimation H Gui, AHJ de Ruiter Journal of Guidance, Control, and Dynamics 41 (4), 863-878, 2018 | 35 | 2018 |
| Attitude tracking of a rigid spacecraft using two internal torques H Gui, G Vukovich, S Xu IEEE Transactions on Aerospace and Electronic Systems 51 (4), 2900-2913, 2015 | 34 | 2015 |
| Adaptive variable-structure finite-time mode control for spacecraft proximity operations with actuator saturation D Lee, G Vukovich, H Gui Advances in Space Research 59 (10), 2473-2487, 2017 | 29 | 2017 |
| On the attitude stabilization of a rigid spacecraft using two skew control moment gyros H Gui, L Jin, S Xu, J Zhang Nonlinear Dynamics 79, 2079-2097, 2015 | 29 | 2015 |
| Local controllability and stabilization of spacecraft attitude by two single-gimbal control moment gyros H Gui, L Jin, S Xu Chinese Journal of Aeronautics 26 (5), 1218-1226, 2013 | 22 | 2013 |
| Attitude stabilization of a spacecraft with two parallel control moment gyroscopes H Gui, G Vukovich, S Xu Journal of Guidance, Control, and Dynamics 39 (3), 728-735, 2016 | 21 | 2016 |
| Robust adaptive spin-axis stabilization of a symmetric spacecraft using two bounded torques H Gui, G Vukovich Advances in Space Research 56 (11), 2495-2507, 2015 | 21 | 2015 |
