High-performance adaptive attitude control of spacecraft with sliding mode disturbance observer
U Javaid, H Dong, S Ijaz, T Alkarkhi, M Haque - IEEE Access, 2022 - ieeexplore.ieee.org
A new disturbance observer-based control method is presented in this paper to address the
attitude tracking problem of rigid-body spacecraft in the presence of external disturbances …
attitude tracking problem of rigid-body spacecraft in the presence of external disturbances …
Distributed adaptive fixed-time formation control for second-order multi-agent systems with collision avoidance
Q Li, J Wei, Q Gou, Z Niu - Information Sciences, 2021 - Elsevier
In this work, the distributed fixed-time formation control problem for a group of second-order
multi-agent systems is investigated with consideration of collision avoidance, external …
multi-agent systems is investigated with consideration of collision avoidance, external …
Adaptive saturated control for spacecraft rendezvous and docking under motion constraints
X Zhao, S Zhang - Aerospace Science and Technology, 2021 - Elsevier
This paper investigates the problem of position tracking and attitude synchronization for
spacecraft rendezvous and docking with a tumbling target, in which kinematic couplings …
spacecraft rendezvous and docking with a tumbling target, in which kinematic couplings …
Fully actuated system approach for 6DOF spacecraft control based on extended state observer
Q Zhao, GR Duan - Journal of Systems Science and Complexity, 2022 - Springer
This paper deals with the problem of position and attitude tracking control for a rigid
spacecraft. A fully actuated system (FAS) model for the six degree-of-freedom (6DOF) …
spacecraft. A fully actuated system (FAS) model for the six degree-of-freedom (6DOF) …
Spacecraft orbital pursuit–evasion games with J2 perturbations and direction-constrained thrust
M Shi, D Ye, Z Sun, W Zhong, H Deng - Acta Astronautica, 2023 - Elsevier
In this paper, we study spacecraft orbital pursuit–evasion games under J 2 perturbations. We
consider that situation where the thrust of each player is constrained and the control …
consider that situation where the thrust of each player is constrained and the control …
Satellite proximate pursuit-evasion game with different thrust configurations
D Ye, M Shi, Z Sun - Aerospace science and technology, 2020 - Elsevier
This paper investigates the proximity satellite pursuit-evasion game where the pursuer
carries three orthogonal thrusters, each of which can exert a magnitude-limited force along …
carries three orthogonal thrusters, each of which can exert a magnitude-limited force along …
Finite-time attitude set-point tracking for thrust-vectoring spacecraft rendezvous
This paper addresses the optimal orbit rendezvous problem for thrust-vectoring spacecraft.
In this scenario, the chaser spacecraft is equipped with only one impulsive thruster fixed in …
In this scenario, the chaser spacecraft is equipped with only one impulsive thruster fixed in …
Continuous constrained attitude regulation of multiple spacecraft on SO (3)
In this paper, both the centralized and distributed attitude regulation of multiple flexible
spacecraft are studied on SO (3) with attitude constraints in the absence of the …
spacecraft are studied on SO (3) with attitude constraints in the absence of the …
Finite-time control for autonomous rendezvous and docking under safe constraint
Y Guo, D Zhang, A Li, S Song, C Wang, Z Liu - Aerospace Science and …, 2021 - Elsevier
The finite-time controller under safe constraint is designed for the non-cooperative space
autonomous rendezvous and docking by using the artificial potential function. To facilitate …
autonomous rendezvous and docking by using the artificial potential function. To facilitate …
Adaptive sliding mode disturbance observer-based control for rendezvous with non-cooperative spacecraft
This paper investigates the tracking and control problem of a spacecraft rendezvous with a
non-cooperative and tumbling space target subject to parametric uncertainty and unknown …
non-cooperative and tumbling space target subject to parametric uncertainty and unknown …