[HTML][HTML] Artificial intelligence for trusted autonomous satellite operations
Abstract Recent advances in Artificial Intelligence (AI) and Cyber-Physical Systems (CPS)
for aerospace applications have brought about new opportunities for the fast-growing …
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 …
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 …
a spacecraft system in close space missions with model uncertainty, unknown disturbance …
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 …
[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 …
tracking) is studied. Firstly, a novel nonsingular terminal sliding mode surface is designed …
Constrained feedback control for spacecraft reorientation with an optimal gain
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 …
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
This article addresses the coupled orbit-attitude tracking problem using low-thrust
propulsion while aiming to minimize on-board spacecraft system communication. An …
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 …
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 …
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 …
formation flying (SFF) systems in the presence of unknown lumped disturbances including …