On the attitude stabilization of a rigid spacecraft using two skew control moment gyros von Gui, Haichao, Jin, Lei, Xu, Shijie, Zhang, Jun

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Adaptive fault‐tolerant spacecraft attitude control using a novel integral terminal sliding mode von Gui, Haichao, Vukovich, George

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Small-time local controllability of spacecraft attitude using control moment gyros von Gui, Haichao, Jin, Lei, Xu, Shijie

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Global finite-time attitude tracking via quaternion feedback von Gui, Haichao, Vukovich, George

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Local controllability and stabilization of spacecraft attitude by two single-gimbal control moment gyros von Gui, Haichao, Jin, Lei, Xu, Shijie

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Finite‐time angular velocity observers for rigid‐body attitude tracking with bounded inputs von Gui, Haichao, Vukovich, George

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Distributed almost global finite-time attitude consensus of multiple spacecraft without velocity measurements von Gui, Haichao, Vukovich, George

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Robust Switching of Modified Rodrigues Parameter Sets for Saturated Global Attitude Control von Gui, Haichao, Vukovich, George

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Adaptive integral sliding mode control for spacecraft attitude tracking with actuator uncertainty von Gui, Haichao, Vukovich, George

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Angular velocity observer design using vector measurements with application to attitude tracking von Zhu, Hangbiao, Gui, Haichao, Su, Wenjie

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Unscented Schmidt-Kalman filter on Lie groups with application to spacecraft attitude estimation von Zhu, Hangbiao, Gui, Haichao, Zhong, Rui

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Gyro-free attitude reorientation control of spacecraft with state and input constraints von Dang, Qingqing, Li, Wenbo, Gui, Haichao

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Robust adaptive spin-axis stabilization of a symmetric spacecraft using two bounded torques von Gui, Haichao, Vukovich, George

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Comments on “Finite-time consensus and collision avoidance control algorithms for multiple AUVs” [Automatica 49 (2013) 3359–3367] von Gui, Haichao, Vukovich, George

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Global finite-time attitude consensus of leader-following spacecraft systems based on distributed observers von Gui, Haichao, de Ruiter, Anton H.J.

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Robustness Analysis and Performance Tuning for the Quaternion Proportional-Derivative Attitude Controller (vol 41, pg 1, 2018) von Gui, Haichao, de Ruiter, Anton H. J.

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Adaptive Fault-Tolerant Spacecraft Pose Tracking With Control Allocation von Gui, Haichao, de Ruiter, Anton H. J.

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Attitude Stabilization of a Spacecraft with Two Parallel Control Moment Gyroscopes von Gui, Haichao, Vukovich, George, Xu, Shijie

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Attitude maneuver control of a two-wheeled spacecraft with bounded wheel speeds von Gui, Haichao, Jin, Lei, Xu, Shijie

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Quaternion Invariant Extended Kalman Filtering for Spacecraft Attitude Estimation von Gui, Haichao, de Ruiter, Anton H J

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