Discrete reconfigurable back-stepping attitude control of reentry hypersonic flight vehicle

Discrete reconfigurable back-stepping attitude control of reentry hypersonic flight vehicle

A discrete reconfigurable back-stepping controller is proposed to resolve the attitude command tracking problem of hypersonic flight vehicle in reentry mode. The hypersonic flight vehicle dynamic equations are transformed into discrete form based on Euler numerical integration method. Discrete contr...

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Bibliographic Details
Main Authors: Zijun Ren, Wenxing Fu, Jie Yan, Bin Xu
Format: Article
Language:English
Published: SAGE Publishing 2017-04-01
Series:Advances in Mechanical Engineering
Online Access:https://doi.org/10.1177/1687814017703900
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spelling doaj-1125b76a5a454f7996795da1aa7cbd6b2020-11-25T02:58:19ZengSAGE PublishingAdvances in Mechanical Engineering1687-81402017-04-01910.1177/1687814017703900Discrete reconfigurable back-stepping attitude control of reentry hypersonic flight vehicleZijun Ren0Wenxing Fu1Jie Yan2Bin Xu3School of Astronautics, Northwestern Polytechnical University, Xi’an, ChinaSchool of Astronautics, Northwestern Polytechnical University, Xi’an, ChinaSchool of Astronautics, Northwestern Polytechnical University, Xi’an, ChinaResearch Institute of Northwestern Polytechnical University in Shenzhen, Shenzhen, ChinaA discrete reconfigurable back-stepping controller is proposed to resolve the attitude command tracking problem of hypersonic flight vehicle in reentry mode. The hypersonic flight vehicle dynamic equations are transformed into discrete form based on Euler numerical integration method. Discrete control command is designed via discrete back-stepping. Control allocation strategy is introduced to deal with the resource distributing problem of reaction control system and aero-surfaces. In computer simulation environment, the vehicle tracks command signals precisely and quickly.https://doi.org/10.1177/1687814017703900
collection DOAJ
language English
format Article
sources DOAJ
author Zijun Ren
Wenxing Fu
Jie Yan
Bin Xu
spellingShingle Zijun Ren
Wenxing Fu
Jie Yan
Bin Xu
Discrete reconfigurable back-stepping attitude control of reentry hypersonic flight vehicle
Advances in Mechanical Engineering
author_facet Zijun Ren
Wenxing Fu
Jie Yan
Bin Xu
author_sort Zijun Ren
title Discrete reconfigurable back-stepping attitude control of reentry hypersonic flight vehicle
title_short Discrete reconfigurable back-stepping attitude control of reentry hypersonic flight vehicle
title_full Discrete reconfigurable back-stepping attitude control of reentry hypersonic flight vehicle
title_fullStr Discrete reconfigurable back-stepping attitude control of reentry hypersonic flight vehicle
title_full_unstemmed Discrete reconfigurable back-stepping attitude control of reentry hypersonic flight vehicle
title_sort discrete reconfigurable back-stepping attitude control of reentry hypersonic flight vehicle
publisher SAGE Publishing
series Advances in Mechanical Engineering
issn 1687-8140
publishDate 2017-04-01
description A discrete reconfigurable back-stepping controller is proposed to resolve the attitude command tracking problem of hypersonic flight vehicle in reentry mode. The hypersonic flight vehicle dynamic equations are transformed into discrete form based on Euler numerical integration method. Discrete control command is designed via discrete back-stepping. Control allocation strategy is introduced to deal with the resource distributing problem of reaction control system and aero-surfaces. In computer simulation environment, the vehicle tracks command signals precisely and quickly.
url https://doi.org/10.1177/1687814017703900
work_keys_str_mv AT zijunren discretereconfigurablebacksteppingattitudecontrolofreentryhypersonicflightvehicle
AT wenxingfu discretereconfigurablebacksteppingattitudecontrolofreentryhypersonicflightvehicle
AT jieyan discretereconfigurablebacksteppingattitudecontrolofreentryhypersonicflightvehicle
AT binxu discretereconfigurablebacksteppingattitudecontrolofreentryhypersonicflightvehicle
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