This article investigates the attitude tracking control of state constrained rigid spacecraft systems with external disturbances. An event-triggered adaptive fuzzy asymptotic backstepping tracking controller is proposed, which makes the spacecraft attitude tracking error asymptotically converge to origin in the presence of inertia uncertainty, external disturbance, and full-state constraints. A novel event-triggered mechanism is established to reduce the waste of communication resources caused by frequent controller updating. A simulation example demonstrates the effectiveness of the control method.
Event-Triggered Adaptive Fuzzy Asymptotic Tracking Control for Rigid Spacecraft Attitude Systems With Full-State Constraints and Disturbances
IEEE Transactions on Aerospace and Electronic Systems ; 60 , 4 ; 3915-3922
01.08.2024
998822 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Event-Triggered Attitude Tracking for Rigid Spacecraft
Springer Verlag | 2021
|Event-triggered adaptive control for attitude tracking of spacecraft
British Library Online Contents | 2019
|Attitude Tracking of Rigid Spacecraft with Uncertainties and Disturbances
Springer Verlag | 2013
|