Adaptive finite-time command filtered fault-tolerant control for uncertain spacecraft with prescribed performance
type: Item
instance of: scholarly article
title: Adaptive finite-time command filtered fault-tolerant control for uncertain spacecraft with prescribed performance
zbMATH Open document ID: 1407.93165
DOI: 10.1155/2018/4912483
author: Xianqiang Yang
published in: Complexity
publication date: 2019-02-19T00:00:00Z
review text: Summary: In this paper, an adaptive finite-time fault-tolerant control scheme is proposed for the attitude stabilization of rigid spacecrafts. A first-order command filter is presented at the second step of the backstepping design to approximate the derivative of the virtual control, such that the singularity problem caused by the differentiation of the virtual control is avoided. Then, an adaptive fuzzy finite-time backstepping controller is developed to achieve the finite-time attitude stabilization subject to inertia uncertainty, external disturbance, actuator saturation, and faults. Through using an error transformation, the prescribed performance boundary is incorporated into the controller design to guarantee the prescribed performance of the system output. Numerical simulations demonstrate the effectiveness of the proposed scheme.
Mathematics Subject Classification ID: 93C40
Mathematics Subject Classification ID: 93B35
Mathematics Subject Classification ID: 93D21
zbMATH DE Number: 7025036
MaRDI profile type: Publication
full work available at URL: https://doi.org/10.1155/2018/4912483
OpenAlex ID: W2899846733
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Wikidata QID: Q128980630
description: scientific article; zbMATH DE number 7025036