H Gui, G Vukovich - … Journal of Robust and Nonlinear Control, 2017 - Wiley Online Library
The attitude tracking of a rigid body without angular velocity measurements is addressed. A continuous angular velocity observer with fractional power functions is proposed to estimate …
N Zhou, X Cheng, Y Xia, Y Liu - IEEE transactions on …, 2020 - ieeexplore.ieee.org
This article investigates the attitude stabilization problem of a rigid spacecraft with actuator saturation and failures. Two neural network-based control schemes are proposed using anti …
There has been an increasing interest in multi-disciplinary research on multisensor attitude estimation technology driven by its versatility and diverse areas of application, such as …
MR Akella, D Thakur, F Mazenc - Journal of Guidance, Control, and …, 2015 - arc.aiaa.org
A smooth angular velocity observer is proposed for the attitude tracking control of a rigid body in the absence of angular velocity measurements. The observer design ensures …
Q Song, W Yu, J Cao, F Liu - IEEE transactions on cybernetics, 2015 - ieeexplore.ieee.org
This paper studies the synchronization problem for a network of coupled harmonic oscillators by proposing a distributed control algorithm based only on delayed position …
This paper is about the construction of a family of centrally synergistic potential functions from a single modified trace function on SO (3). First, we demonstrate that it is possible to …
Z Zheng, M Shen - Aerospace Science and Technology, 2019 - Elsevier
Abstract for multiple spacecraft with actuator and angular velocity constraints using vector measurements directly. First, the novel vector measurements-based cooperative attitude …
L Benziane, A El Hadri, A Seba… - … on Control Systems …, 2016 - ieeexplore.ieee.org
This brief proposes new algorithms for attitude estimation and control, based on fused inertial vector measurements using a linear complementary filters principle. First, n-order …
LG Gong, Q Wang, CY Dong - Journal of the Franklin Institute, 2019 - Elsevier
This paper investigates spacecraft output feedback attitude control problem based on extended state observer (ESO) and adaptive dynamic programming (ADP) approach. For …