Fault estimation and compensation for hypersonic flight vehicle via type-2 fuzzy technique and cuckoo search algorithm

This study proposes a fault estimation and compensation scheme for hypersonic flight vehicle (HFV) attitude system with body flap fault. To achieve the fault compensation capability, an interval type-2 fuzzy estimator is designed to approximate the unknown nonlinear function caused by modeling uncer...

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Bibliographic Details
Main Authors: Ang Wang, Huajun Gong, Fuyang Chen
Format: Article
Language:English
Published: SAGE Publishing 2020-01-01
Series:International Journal of Advanced Robotic Systems
Online Access:https://doi.org/10.1177/1729881419891605
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spelling doaj-9fe3bf79b47e4a4a9002841f0d24aaa22020-11-25T03:40:36ZengSAGE PublishingInternational Journal of Advanced Robotic Systems1729-88142020-01-011710.1177/1729881419891605Fault estimation and compensation for hypersonic flight vehicle via type-2 fuzzy technique and cuckoo search algorithmAng WangHuajun GongFuyang ChenThis study proposes a fault estimation and compensation scheme for hypersonic flight vehicle (HFV) attitude system with body flap fault. To achieve the fault compensation capability, an interval type-2 fuzzy estimator is designed to approximate the unknown nonlinear function caused by modeling uncertainties and the fault. The fault-tolerant controller via the terminal sliding mode and dynamic surface techniques is developed to ensure the tracking accuracy of attitude angles for HFV and the desired control torque can be achieved. Then, a novel control allocation scheme with a cuckoo search algorithm and linear programming method is proposed to distribute the desired torque to aerodynamic surfaces and reaction control system jets. The stability of the proposed scheme is analyzed using the Lyapunov stability theory. The validity of the method is verified by a series of comparisons on numerical simulation results.https://doi.org/10.1177/1729881419891605
collection DOAJ
language English
format Article
sources DOAJ
author Ang Wang
Huajun Gong
Fuyang Chen
spellingShingle Ang Wang
Huajun Gong
Fuyang Chen
Fault estimation and compensation for hypersonic flight vehicle via type-2 fuzzy technique and cuckoo search algorithm
International Journal of Advanced Robotic Systems
author_facet Ang Wang
Huajun Gong
Fuyang Chen
author_sort Ang Wang
title Fault estimation and compensation for hypersonic flight vehicle via type-2 fuzzy technique and cuckoo search algorithm
title_short Fault estimation and compensation for hypersonic flight vehicle via type-2 fuzzy technique and cuckoo search algorithm
title_full Fault estimation and compensation for hypersonic flight vehicle via type-2 fuzzy technique and cuckoo search algorithm
title_fullStr Fault estimation and compensation for hypersonic flight vehicle via type-2 fuzzy technique and cuckoo search algorithm
title_full_unstemmed Fault estimation and compensation for hypersonic flight vehicle via type-2 fuzzy technique and cuckoo search algorithm
title_sort fault estimation and compensation for hypersonic flight vehicle via type-2 fuzzy technique and cuckoo search algorithm
publisher SAGE Publishing
series International Journal of Advanced Robotic Systems
issn 1729-8814
publishDate 2020-01-01
description This study proposes a fault estimation and compensation scheme for hypersonic flight vehicle (HFV) attitude system with body flap fault. To achieve the fault compensation capability, an interval type-2 fuzzy estimator is designed to approximate the unknown nonlinear function caused by modeling uncertainties and the fault. The fault-tolerant controller via the terminal sliding mode and dynamic surface techniques is developed to ensure the tracking accuracy of attitude angles for HFV and the desired control torque can be achieved. Then, a novel control allocation scheme with a cuckoo search algorithm and linear programming method is proposed to distribute the desired torque to aerodynamic surfaces and reaction control system jets. The stability of the proposed scheme is analyzed using the Lyapunov stability theory. The validity of the method is verified by a series of comparisons on numerical simulation results.
url https://doi.org/10.1177/1729881419891605
work_keys_str_mv AT angwang faultestimationandcompensationforhypersonicflightvehicleviatype2fuzzytechniqueandcuckoosearchalgorithm
AT huajungong faultestimationandcompensationforhypersonicflightvehicleviatype2fuzzytechniqueandcuckoosearchalgorithm
AT fuyangchen faultestimationandcompensationforhypersonicflightvehicleviatype2fuzzytechniqueandcuckoosearchalgorithm
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