Haichao Gui

Publication Activity (10 Years)

Years Active: 2015-2024
Publications (10 Years): 11

Top Topics

Nonrigid Objects

Top Venues

IEEE Trans. Control. Syst. Technol.

IEEE Trans. Aerosp. Electron. Syst.

Publications

Hangbiao Zhu, Zhongxiang Xie, Haichao Gui
Global Pose and Velocity-Bias Observer Design on SE(3) Using Synergistic-Based Hybrid Method. ECC (2024)
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) (2021)
Haichao Gui
Observer-Based Fault-Tolerant Spacecraft Attitude Tracking Using Sequential Lyapunov Analyses. IEEE Trans. Autom. Control. 66 (12) (2021)
Haichao Gui
Observer-Based Fault-Tolerant Spacecraft Attitude Tracking Using Sequential Lyapunov Analyses. CoRR (2020)
Haichao Gui, Anton H. J. de Ruiter
Adaptive Fault-Tolerant Spacecraft Pose Tracking With Control Allocation. IEEE Trans. Control. Syst. Technol. 27 (2) (2019)
Haichao Gui, Anton H. J. de Ruiter
Global finite-time attitude consensus of leader-following spacecraft systems based on distributed observers. Autom. 91 (2018)
Haichao Gui, George Vukovich
Comments on "Finite-time consensus and collision avoidance control algorithms for multiple AUVs" [Automatica 49 (2013) 3359-3367]. Autom. 75 (2017)
George Vukovich, Haichao Gui
Robust Adaptive Tracking of Rigid-Body Motion With Applications to Asteroid Proximity Operations. IEEE Trans. Aerosp. Electron. Syst. 53 (1) (2017)
Haichao Gui, George Vukovich
Global Finite-Time Attitude Tracking via Quaternion Feedback. CoRR (2016)
Haichao Gui, George Vukovich
Finite-time output-feedback position and attitude tracking of a rigid body. Autom. 74 (2016)
Haichao Gui, George Vukovich
Global finite-time attitude tracking via quaternion feedback. Syst. Control. Lett. 97 (2016)
Haichao Gui, George Vukovich
Adaptive integral sliding mode control for spacecraft attitude tracking with actuator uncertainty. J. Frankl. Inst. 352 (12) (2015)
Haichao Gui, George Vukovich, Shijie Xu
Attitude tracking of a rigid spacecraft using two internal torques. IEEE Trans. Aerosp. Electron. Syst. 51 (4) (2015)
Haichao Gui, Lei Jin, Shijie Xu
Small-time local controllability of spacecraft attitude using control moment gyros. Autom. 53 (2015)