Adaptive backstepping finite time attitude control of reentry RLV with input constraint
type: Item
instance of: scholarly article
title: Adaptive backstepping finite time attitude control of reentry RLV with input constraint
zbMATH Open document ID: 1407.93180
DOI: 10.1155/2014/801747
author: Fang Wang
author: Qun Zong
author: Bailing Tian
published in: Mathematical Problems in Engineering
publication date: 2019-02-08T00:00:00Z
review text: Summary: This paper presents the finite time attitude tracking control problem of reusable launch vehicle (RLV) in reentry phase under input constraint, model uncertainty, and external disturbance. A control-oriented model of rotational dynamics is developed and used for controller design for the complex coupling of the translational and rotational dynamics. Firstly, fast terminal sliding mode control is incorporated into backstepping control to design controller considering model uncertainty and external disturbance. The ``explosion of terms'' problem inherent in backstepping control is eliminated by a robust second order filter. Secondly, the control problem in the presence of input constraint is further considered, and a constrained adaptive backstepping fast terminal sliding mode control scheme is developed. At the control design level, adaptive law is employed to estimate the unknown norm bound of lumped uncertainty with the reduction of computational burden. The Lyapunov-based stability analysis of the closed-loop system is carried out. The control performance is presented via the simulation of six-degree-of-freedom (6-DOF) model of RLV.
Mathematics Subject Classification ID: 93C40
Mathematics Subject Classification ID: 93B12
zbMATH DE Number: 7017291
MaRDI profile type: Publication
full work available at URL: https://doi.org/10.1155/2014/801747
OpenAlex ID: W1993274049
Wikidata QID: Q59069330
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description: scientific article; zbMATH DE number 7017291