This paper considers the problem of attitude tracking control for uncertain rigid spacecraft subject to control input magnitude and rate saturation (MRS). First, a smooth input MRS model is proposed. Then, a robust attitude tracking control scheme is designed based on the backstepping and finite-time disturbance observer techniques. Finally, the effectiveness of the control scheme derived here is illustrated by numerical simulations.
Disturbance Observer-Based Attitude Control for Spacecraft With Input MRS
IEEE Transactions on Aerospace and Electronic Systems ; 55 , 1 ; 384-396
01.02.2019
3684084 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Disturbance observer based finite-time attitude control for rigid spacecraft under input saturation
Online Contents | 2014
|Fuzzy Disturbance Observer Based NTSM Attitude Control for Combined Spacecraft
Springer Verlag | 2023
|