Deriving a Control-Oriented Model for an Axisymmetric Vehicle With the Power-Law Revolution Nose

Detalhes bibliográficos
Autor(a) principal: Huang,Jun
Data de Publicação: 2020
Outros Autores: Liu,Zhigui, Liu,Zhiqin, Wang,Qingfeng, Fu,Jie
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Journal of Aerospace Technology and Management (Online)
Texto Completo: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462020000100337
Resumo: ABSTRACT: The purpose of this paper is to construct a new general vehicle model as an open fundamental material for the guidance and control research. In this study, parameterized configuration, aerodynamics calculation, control-oriented modeling, stability analysis, and nominal trajectory design are performed for the general vehicle model. First, the aerodynamic configuration is parameterized as an axisymmetric body with a power-law revolution nose. Then, an engineering method considering inviscid flow, base drag and skin friction is used for the aerodynamics calculation, and a control-oriented fitting model of longitudinal aerodynamics is established based on the analysis of the correlation between aerodynamic force and the parameters of Mach number, attack angle, elevator deflection and height. Next, the aerothermodynamic environment prediction of power-law revolution axisymmetric hypersonic vehicle (PRAHV) is discussed, and the nose heating rate formula of PRAHV is established. The stability analysis and nominal trajectory design of PRAHV is performed based on the fitting model and the heating rate formula. The stability analysis shows that both the static stability and dynamic stability of the vehicle are unstable. The nominal trajectory of unpowered longitudinal maneuvering is achieved by the hp-adaptive pseudospectral method, which demonstrated that the availability of the control-oriented model established in this paper. In conclusion, this work provides a fundamental object for further study of vehicle guidance, control, and evaluation.
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spelling Deriving a Control-Oriented Model for an Axisymmetric Vehicle With the Power-Law Revolution NoseKinzhal-like systemAerodynamic engineering calculationControl-oriented modelingModel stability analysisNominal trajectoryABSTRACT: The purpose of this paper is to construct a new general vehicle model as an open fundamental material for the guidance and control research. In this study, parameterized configuration, aerodynamics calculation, control-oriented modeling, stability analysis, and nominal trajectory design are performed for the general vehicle model. First, the aerodynamic configuration is parameterized as an axisymmetric body with a power-law revolution nose. Then, an engineering method considering inviscid flow, base drag and skin friction is used for the aerodynamics calculation, and a control-oriented fitting model of longitudinal aerodynamics is established based on the analysis of the correlation between aerodynamic force and the parameters of Mach number, attack angle, elevator deflection and height. Next, the aerothermodynamic environment prediction of power-law revolution axisymmetric hypersonic vehicle (PRAHV) is discussed, and the nose heating rate formula of PRAHV is established. The stability analysis and nominal trajectory design of PRAHV is performed based on the fitting model and the heating rate formula. The stability analysis shows that both the static stability and dynamic stability of the vehicle are unstable. The nominal trajectory of unpowered longitudinal maneuvering is achieved by the hp-adaptive pseudospectral method, which demonstrated that the availability of the control-oriented model established in this paper. In conclusion, this work provides a fundamental object for further study of vehicle guidance, control, and evaluation.Departamento de Ciência e Tecnologia Aeroespacial2020-01-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462020000100337Journal of Aerospace Technology and Management v.12 2020reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v12.1164info:eu-repo/semantics/openAccessHuang,JunLiu,ZhiguiLiu,ZhiqinWang,QingfengFu,Jieeng2020-09-14T00:00:00Zoai:scielo:S2175-91462020000100337Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2020-09-14T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Deriving a Control-Oriented Model for an Axisymmetric Vehicle With the Power-Law Revolution Nose
title Deriving a Control-Oriented Model for an Axisymmetric Vehicle With the Power-Law Revolution Nose
spellingShingle Deriving a Control-Oriented Model for an Axisymmetric Vehicle With the Power-Law Revolution Nose
Huang,Jun
Kinzhal-like system
Aerodynamic engineering calculation
Control-oriented modeling
Model stability analysis
Nominal trajectory
title_short Deriving a Control-Oriented Model for an Axisymmetric Vehicle With the Power-Law Revolution Nose
title_full Deriving a Control-Oriented Model for an Axisymmetric Vehicle With the Power-Law Revolution Nose
title_fullStr Deriving a Control-Oriented Model for an Axisymmetric Vehicle With the Power-Law Revolution Nose
title_full_unstemmed Deriving a Control-Oriented Model for an Axisymmetric Vehicle With the Power-Law Revolution Nose
title_sort Deriving a Control-Oriented Model for an Axisymmetric Vehicle With the Power-Law Revolution Nose
author Huang,Jun
author_facet Huang,Jun
Liu,Zhigui
Liu,Zhiqin
Wang,Qingfeng
Fu,Jie
author_role author
author2 Liu,Zhigui
Liu,Zhiqin
Wang,Qingfeng
Fu,Jie
author2_role author
author
author
author
dc.contributor.author.fl_str_mv Huang,Jun
Liu,Zhigui
Liu,Zhiqin
Wang,Qingfeng
Fu,Jie
dc.subject.por.fl_str_mv Kinzhal-like system
Aerodynamic engineering calculation
Control-oriented modeling
Model stability analysis
Nominal trajectory
topic Kinzhal-like system
Aerodynamic engineering calculation
Control-oriented modeling
Model stability analysis
Nominal trajectory
description ABSTRACT: The purpose of this paper is to construct a new general vehicle model as an open fundamental material for the guidance and control research. In this study, parameterized configuration, aerodynamics calculation, control-oriented modeling, stability analysis, and nominal trajectory design are performed for the general vehicle model. First, the aerodynamic configuration is parameterized as an axisymmetric body with a power-law revolution nose. Then, an engineering method considering inviscid flow, base drag and skin friction is used for the aerodynamics calculation, and a control-oriented fitting model of longitudinal aerodynamics is established based on the analysis of the correlation between aerodynamic force and the parameters of Mach number, attack angle, elevator deflection and height. Next, the aerothermodynamic environment prediction of power-law revolution axisymmetric hypersonic vehicle (PRAHV) is discussed, and the nose heating rate formula of PRAHV is established. The stability analysis and nominal trajectory design of PRAHV is performed based on the fitting model and the heating rate formula. The stability analysis shows that both the static stability and dynamic stability of the vehicle are unstable. The nominal trajectory of unpowered longitudinal maneuvering is achieved by the hp-adaptive pseudospectral method, which demonstrated that the availability of the control-oriented model established in this paper. In conclusion, this work provides a fundamental object for further study of vehicle guidance, control, and evaluation.
publishDate 2020
dc.date.none.fl_str_mv 2020-01-01
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462020000100337
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462020000100337
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.v12.1164
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv text/html
dc.publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
dc.source.none.fl_str_mv Journal of Aerospace Technology and Management v.12 2020
reponame:Journal of Aerospace Technology and Management (Online)
instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
instname_str Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron_str DCTA
institution DCTA
reponame_str Journal of Aerospace Technology and Management (Online)
collection Journal of Aerospace Technology and Management (Online)
repository.name.fl_str_mv Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
repository.mail.fl_str_mv ||secretary@jatm.com.br
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