[HTML][HTML] Artificial intelligence for trusted autonomous satellite operations

K Thangavel, R Sabatini, A Gardi, K Ranasinghe… - Progress in Aerospace …, 2024 - Elsevier
Abstract Recent advances in Artificial Intelligence (AI) and Cyber-Physical Systems (CPS)
for aerospace applications have brought about new opportunities for the fast-growing …

Fixed-time formation control for spacecraft with prescribed performance guarantee under input saturation

M Zhuang, L Tan, K Li, S Song - Aerospace Science and Technology, 2021 - Elsevier
This paper investigates the fixed-time stability of spacecraft formation flying by considering
input saturation and prescribed performance constraints, including the safe distance …

Adaptive control on SE (3) for spacecraft pose tracking with harmonic disturbance and input saturation

H Zhang, D Ye, Y **ao, Z Sun - IEEE Transactions on …, 2022 - ieeexplore.ieee.org
This article investigates the coupled attitude and orbit tracking maneuver control problem of
a spacecraft system in close space missions with model uncertainty, unknown disturbance …

Finite-time attitude set-point tracking for thrust-vectoring spacecraft rendezvous

J Zhang, JD Biggs, D Ye, Z Sun - Aerospace Science and Technology, 2020 - Elsevier
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 …

[HTML][HTML] Fixed-time position coordinated tracking control for spacecraft formation flying with collision avoidance

M Zhuang, TAN Liguo, LI Kehang, S Shenmin - Chinese Journal of …, 2021 - Elsevier
In this paper, the fixed-time stability of spacecraft formation reconfiguration (position
tracking) is studied. Firstly, a novel nonsingular terminal sliding mode surface is designed …

Constrained feedback control for spacecraft reorientation with an optimal gain

B Li, Y Wang, K Zhang, GR Duan - IEEE Transactions on …, 2021 - ieeexplore.ieee.org
This article addresses the problem of spacecraft reorientation subject to attitude pointing,
angular velocity, and actuator constraints. In order to tackle the attitude pointing constraints …

Extended-state-observer-based event-triggered orbit-attitude tracking for low-thrust spacecraft

J Zhang, JD Biggs, D Ye, Z Sun - IEEE Transactions on …, 2019 - ieeexplore.ieee.org
This article addresses the coupled orbit-attitude tracking problem using low-thrust
propulsion while aiming to minimize on-board spacecraft system communication. An …

Coupled Dynamics and Integrated Control for position and attitude motions of spacecraft: a survey

F Zhang, G Duan - IEEE/CAA journal of Automatica sinica, 2023 - ieeexplore.ieee.org
Inspired by the integrated guidance and control design for endo-atmospheric aircraft, the
integrated position and attitude control of spacecraft has attracted increasing attention and …

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 …

Robust attitude consensus control for multiple spacecraft systems with unknown disturbances via variable structure control and adaptive sliding mode control

X **e, T Sheng, L He - Advances in Space Research, 2022 - Elsevier
This paper addresses the robust attitude consensus tracking problem for spacecraft
formation flying (SFF) systems in the presence of unknown lumped disturbances including …