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Adaptive output feedback attitude control for reusable launch vehicle with input constraints and actuator faults.

Authors :
Li, Wenting
Zhao, Jinsong
Su, Shanwei
Mo, Ran
Lin, Yan
Source :
Aerospace Science & Technology. Nov2023:Part A, Vol. 142, pN.PAG-N.PAG. 1p.
Publication Year :
2023

Abstract

This paper considers an adaptive output feedback fault tolerant control (FTC) for a reusable launch vehicle (RLV) during reentry phase for which four grid fins are used as actuators. Based on a prescribed tracking performance and an auxiliary system to deal with the input constraints, the proposed adaptive controller can compensate for the effect of uncertainties, external and internal disturbances, input constraints and actuator faults. It is shown that with the proposed scheme, the system tracking performance can be guaranteed even in the presence multiple actuator faults. The influence of the input constraints on the tracking performance is also investigated. Simulation results are presented to illustrate the effectiveness of the proposed scheme. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
12709638
Volume :
142
Database :
Academic Search Index
Journal :
Aerospace Science & Technology
Publication Type :
Academic Journal
Accession number :
173889325
Full Text :
https://doi.org/10.1016/j.ast.2023.108616