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contributor authorZhang Xiu-yun;Zong Qun;Tian Bai-ling;Shao Shi-kai;Liu Wen-jing
date accessioned2019-02-26T07:37:41Z
date available2019-02-26T07:37:41Z
date issued2018
identifier other%28ASCE%29AS.1943-5525.0000915.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4248366
description abstractThis paper investigates a fault tolerant problem for the rigid spacecraft in the presence of additive faults and nonlinear disturbances. An adaptive observer and an adaptive terminal sliding mode observer (ATSMO) are presented respectively to distinguish the faults and external disturbances in finite time. Then, we develop a novel finite-time continuous terminal sliding mode controller (CTSMC) to compensate the detected faults. Unlike most of the existing online fault estimation, the proposed approach could achieve finite-time reconstruction of unknown faults and disturbances simultaneously, while the upper bound knowledge is unnecessary. Moreover, the proposed finite-time fault-tolerant controller (FTC) is only based on the information of available output and its first derivative. The effectiveness of the proposed methodology is demonstrated by simulation results.
publisherAmerican Society of Civil Engineers
titleFinite-Time Fault Estimation and Fault-Tolerant Control for Rigid Spacecraft
typeJournal Paper
journal volume31
journal issue6
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000915
page4018091
treeJournal of Aerospace Engineering:;2018:;Volume ( 031 ):;issue: 006
contenttypeFulltext


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