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Haichao Gui
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2020 – today
- 2024
- [c1]Hangbiao Zhu, Zhongxiang Xie, Haichao Gui:
Global Pose and Velocity-Bias Observer Design on SE(3) Using Synergistic-Based Hybrid Method. ECC 2024: 1752-1757 - 2021
- [j11]Haichao Gui
:
Observer-Based Fault-Tolerant Spacecraft Attitude Tracking Using Sequential Lyapunov Analyses. IEEE Trans. Autom. Control. 66(12): 6108-6114 (2021) - [j10]Haichao Gui
, Yong Wang
, Wenjie Su
:
Hybrid Global Finite-Time Dual-Quaternion Observer and Controller for Velocity-Free Spacecraft Pose Tracking. IEEE Trans. Control. Syst. Technol. 29(5): 2129-2141 (2021) - 2020
- [i2]Haichao Gui:
Observer-Based Fault-Tolerant Spacecraft Attitude Tracking Using Sequential Lyapunov Analyses. CoRR abs/2009.06241 (2020)
2010 – 2019
- 2019
- [j9]Haichao Gui
, Anton H. J. de Ruiter
:
Adaptive Fault-Tolerant Spacecraft Pose Tracking With Control Allocation. IEEE Trans. Control. Syst. Technol. 27(2): 479-494 (2019) - 2018
- [j8]Haichao Gui, Anton H. J. de Ruiter:
Global finite-time attitude consensus of leader-following spacecraft systems based on distributed observers. Autom. 91: 225-232 (2018) - 2017
- [j7]Haichao Gui, George Vukovich:
Comments on "Finite-time consensus and collision avoidance control algorithms for multiple AUVs" [Automatica 49 (2013) 3359-3367]. Autom. 75: 75-76 (2017) - [j6]George Vukovich, Haichao Gui:
Robust Adaptive Tracking of Rigid-Body Motion With Applications to Asteroid Proximity Operations. IEEE Trans. Aerosp. Electron. Syst. 53(1): 419-430 (2017) - 2016
- [j5]Haichao Gui, George Vukovich:
Finite-time output-feedback position and attitude tracking of a rigid body. Autom. 74: 270-278 (2016) - [j4]Haichao Gui, George Vukovich:
Global finite-time attitude tracking via quaternion feedback. Syst. Control. Lett. 97: 176-183 (2016) - [i1]Haichao Gui, George Vukovich:
Global Finite-Time Attitude Tracking via Quaternion Feedback. CoRR abs/1602.06492 (2016) - 2015
- [j3]Haichao Gui, Lei Jin, Shijie Xu:
Small-time local controllability of spacecraft attitude using control moment gyros. Autom. 53: 141-148 (2015) - [j2]Haichao Gui, George Vukovich:
Adaptive integral sliding mode control for spacecraft attitude tracking with actuator uncertainty. J. Frankl. Inst. 352(12): 5832-5852 (2015) - [j1]Haichao Gui, George Vukovich, Shijie Xu:
Attitude tracking of a rigid spacecraft using two internal torques. IEEE Trans. Aerosp. Electron. Syst. 51(4): 2900-2913 (2015)
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