Haichao Gui

According to our database, Haichao Gui authored at least 13 papers between 2015 and 2024.

Collaborative distances:

• Dijkstra number of four.
• Erdős number of five.

2024

Attitude Estimation via Matrix Fisher Distributions on SO(3) Using Non-Unit Vector Measurements.

Shijie Wang, Haichao Gui, Rui Zhong

CoRR, 2024

Global Pose and Velocity-Bias Observer Design on SE(3) Using Synergistic-Based Hybrid Method.

Hangbiao Zhu, Zhongxiang Xie, Haichao Gui

Proceedings of the European Control Conference, 2024

2021

Hybrid Global Finite-Time Dual-Quaternion Observer and Controller for Velocity-Free Spacecraft Pose Tracking.

Haichao Gui, Yong Wang, Wenjie Su

IEEE Trans. Control. Syst. Technol., 2021

Observer-Based Fault-Tolerant Spacecraft Attitude Tracking Using Sequential Lyapunov Analyses.

Haichao Gui

IEEE Trans. Autom. Control., 2021

2019

Adaptive Fault-Tolerant Spacecraft Pose Tracking With Control Allocation.

Haichao Gui, Anton H. J. de Ruiter

IEEE Trans. Control. Syst. Technol., 2019

2018

Global finite-time attitude consensus of leader-following spacecraft systems based on distributed observers.

Haichao Gui, Anton H. J. de Ruiter

Autom., 2018

2017

Robust Adaptive Tracking of Rigid-Body Motion With Applications to Asteroid Proximity Operations.

George Vukovich, Haichao Gui

IEEE Trans. Aerosp. Electron. Syst., 2017

Comments on "Finite-time consensus and collision avoidance control algorithms for multiple AUVs" [Automatica 49 (2013) 3359-3367].

Haichao Gui, George Vukovich

Autom., 2017

2016

Global finite-time attitude tracking via quaternion feedback.

Haichao Gui, George Vukovich

Syst. Control. Lett., 2016

Finite-time output-feedback position and attitude tracking of a rigid body.

Haichao Gui, George Vukovich

Autom., 2016

2015

Attitude tracking of a rigid spacecraft using two internal torques.

Haichao Gui, George Vukovich, Shijie Xu

IEEE Trans. Aerosp. Electron. Syst., 2015

Adaptive integral sliding mode control for spacecraft attitude tracking with actuator uncertainty.

Haichao Gui, George Vukovich

J. Frankl. Inst., 2015

Small-time local controllability of spacecraft attitude using control moment gyros.

Haichao Gui, Lei Jin, Shijie Xu

Autom., 2015