Composite Practically Fixed Time Controller Design for a Hypersonic Vehicle With Multisource Uncertainty and Actuator Fault

This article addresses the tracking control problem of a hypersonic vehicle subject to multisource uncertainty and actuator fault. A composite fixed time control scheme is designed to achieve the stable tracking of velocity and altitude in fixed time. A nonsingular fast terminal sliding mode control...

Full description

Saved in:
Bibliographic Details
Published inIEEE transactions on aerospace and electronic systems Vol. 57; no. 6; pp. 4375 - 4389
Main Authors Wang, Fang, Li, Yaping, Zhou, Chao, Zong, Qun, Hua, Changchun
Format Journal Article
LanguageEnglish
Published New York IEEE 01.12.2021
The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subjects
Actuators
Aerodynamics
Altitude
Atmospheric modeling
Control systems design
Controllers
Disturbance observers
Fast fixed time filter (FFTF)
fixed-time disturbance observer (FTDO)
hypersonic vehicle (HSV)
Hypersonic vehicles
Mathematical model
nonsingular fast terminal sliding mode controller
practically fixed time control
Sliding mode control
Stability
Stability analysis
Subsystems
Tracking control
Tracking errors
Uncertainty
Vehicle dynamics
Online AccessGet full text

Cover

Abstract This article addresses the tracking control problem of a hypersonic vehicle subject to multisource uncertainty and actuator fault. A composite fixed time control scheme is designed to achieve the stable tracking of velocity and altitude in fixed time. A nonsingular fast terminal sliding mode controller and a practically fixed-time backstepping controller are, respectively, developed for velocity subsystem and altitude subsystem. Fixed-time disturbance observer is used to tackle lumped uncertainties and a new fast fixed time filter is constructed to avoid the “explosion of terms” problem. Then, the fixed-time stability of velocity tracking error and the practically fixed-time stability of altitude tracking error are proved. Finally, compared simulations are carried out to present the efficiency of the designed control scheme.
AbstractList This article addresses the tracking control problem of a hypersonic vehicle subject to multisource uncertainty and actuator fault. A composite fixed time control scheme is designed to achieve the stable tracking of velocity and altitude in fixed time. A nonsingular fast terminal sliding mode controller and a practically fixed-time backstepping controller are, respectively, developed for velocity subsystem and altitude subsystem. Fixed-time disturbance observer is used to tackle lumped uncertainties and a new fast fixed time filter is constructed to avoid the “explosion of terms” problem. Then, the fixed-time stability of velocity tracking error and the practically fixed-time stability of altitude tracking error are proved. Finally, compared simulations are carried out to present the efficiency of the designed control scheme.
Author Zhou, Chao
Wang, Fang
Zong, Qun
Hua, Changchun
Li, Yaping
Author_xml – sequence: 1
  givenname: Fang
  orcidid: 0000-0002-8180-7839
  surname: Wang
  fullname: Wang, Fang
  email: wangfang@ysu.edu.cn
  organization: Yanshan University, Qinhuangdao, China
– sequence: 2
  givenname: Yaping
  surname: Li
  fullname: Li, Yaping
  email: 2990819068@qq.com
  organization: Yanshan University, Qinhuangdao, China
– sequence: 3
  givenname: Chao
  orcidid: 0000-0001-9740-4367
  surname: Zhou
  fullname: Zhou, Chao
  email: zhouchao@hebau.edu.cn
  organization: Hebei Agricultural University, Qinhuangdao, China
– sequence: 4
  givenname: Qun
  orcidid: 0000-0003-0734-6728
  surname: Zong
  fullname: Zong, Qun
  email: zongqun@tju.edu.cn
  organization: Tianjin University, Tianjin, China
– sequence: 5
  givenname: Changchun
  orcidid: 0000-0001-6311-2112
  surname: Hua
  fullname: Hua, Changchun
  email: cch@ysu.edu.cn
  organization: Yanshan University, Qinhuangdao, China
BookMark eNp9kE1LAzEQhoNUsK3-APES8Lw1H_uVY6mtFSoKtnpcstlZm7JNapKCxT_vLi0ePHgaBt5n3uEZoJ6xBhC6pmREKRF3y_H0dcQIoyNOCWc8O0N9miRZJFLCe6hPCM0jwRJ6gQbeb9o1zmPeR98Tu91ZrwPgFydV0Eo2zQHP9BdUeKm3gCfWBGebBhy-B68_DK6twxLPDztw3hqt8BustWoAv-uwxk_7Jmhv904BXhkFLkhtwgFLU-GxCnsZWnwm29QlOq9l4-HqNIdoNZsuJ_No8fzwOBkvIsUED1HMgSW5yqFUWVmJnArIY6bKWpQ5VbyM07pStAaiMoAUBClTTmJayazqEjEfotvj3Z2zn3vwodi075m2smApSTKSsjRtU_SYUs5676Audk5vpTsUlBSd46JzXHSOi5Pjlsn-MEoHGXSnTOrmX_LmSGoA-G0SCWWxIPwHTr-Nmg
CODEN IEARAX
CitedBy_id crossref_primary_10_1017_aer_2023_116
crossref_primary_10_1109_TAES_2023_3274098
crossref_primary_10_1109_TAES_2022_3227886
crossref_primary_10_1002_rnc_6722
crossref_primary_10_1016_j_ast_2023_108773
crossref_primary_10_1109_TAES_2024_3442162
crossref_primary_10_1177_01423312241239419
crossref_primary_10_1016_j_isatra_2023_06_013
crossref_primary_10_1360_SSI_2023_0285
crossref_primary_10_1109_TAES_2023_3331345
crossref_primary_10_1016_j_ast_2023_108517
crossref_primary_10_1109_TAES_2022_3160687
crossref_primary_10_1016_j_apm_2024_01_044
crossref_primary_10_1155_2022_5419377
crossref_primary_10_1016_j_biosystemseng_2024_06_013
crossref_primary_10_1002_rnc_7864
crossref_primary_10_1016_j_jfranklin_2024_107500
crossref_primary_10_1177_01423312221147950
Cites_doi 10.2514/6.2010-8285
10.1007/s11071-017-3824-3
10.3724/SP.J.1004.2013.01901
10.1002/acs.2664
10.1109/TAC.2011.2160030
10.1109/TASE.2020.3008846
10.1109/TII.2019.2914478
10.1049/iet-cta.2016.1256
10.2514/1.G002777
10.1109/TFUZZ.2019.2934934
10.1109/TAES.2020.3040519
10.2514/1.23370
10.2514/1.J054428
10.2514/1.57739
10.1016/j.ins.2019.08.012
10.1109/TSMC.2018.2847706
10.1109/ACC.2009.5160211
10.2514/1.27830
10.2514/6.2009-5601
10.2514/1.39210
10.1109/TAC.2011.2179869
10.2514/6.2003-7081
10.1016/j.actaastro.2019.07.041
10.1016/j.ast.2021.106554
10.1109/TIE.2013.2271597
10.1016/j.isatra.2018.12.043
10.2514/3.21349
10.2514/6.2007-6396
10.1109/TII.2019.2945861
10.1049/iet-cta.2016.1457
10.1109/TIE.2015.2442224
10.1109/TIE.2017.2739700
10.1016/j.automatica.2015.01.021
10.1109/TSMC.2018.2837378
10.2514/6.2016-1325
10.1109/TAC.2021.3053194
10.1109/TAES.2020.2999149
10.1109/TAC.2016.2600343
10.1109/CDC.2008.4739001
10.1016/j.ast.2019.105608
10.2514/6.2011-6227
10.1016/j.jfranklin.2018.01.042
10.1109/TCST.2016.2603072
10.2514/6.2004-4805
10.1080/00207179.2016.1207101
10.2514/6.2007-6626
10.1109/TCYB.2018.2794972
10.1049/iet-cta.2018.5482
10.1016/j.neucom.2015.08.017
10.1109/TAC.2021.3059689
10.1109/TIE.2017.2701776
10.1109/ACCESS.2019.2900252
ContentType Journal Article
Copyright Copyright The Institute of Electrical and Electronics Engineers, Inc. (IEEE) 2021
Copyright_xml – notice: Copyright The Institute of Electrical and Electronics Engineers, Inc. (IEEE) 2021
DBID 97E
RIA
RIE
AAYXX
CITATION
7SP
7TB
8FD
FR3
H8D
L7M
DOI 10.1109/TAES.2021.3103237
DatabaseName IEEE All-Society Periodicals Package (ASPP) 2005–Present
IEEE All-Society Periodicals Package (ASPP) 1998–Present
IEEE Electronic Library (IEL)
CrossRef
Electronics & Communications Abstracts
Mechanical & Transportation Engineering Abstracts
Technology Research Database
Engineering Research Database
Aerospace Database
Advanced Technologies Database with Aerospace
DatabaseTitle CrossRef
Aerospace Database
Engineering Research Database
Technology Research Database
Mechanical & Transportation Engineering Abstracts
Advanced Technologies Database with Aerospace
Electronics & Communications Abstracts
DatabaseTitleList
Aerospace Database
Database_xml – sequence: 1
  dbid: RIE
  name: IEEE Electronic Library (IEL)
  url: https://proxy.k.utb.cz/login?url=https://ieeexplore.ieee.org/
  sourceTypes: Publisher
DeliveryMethod fulltext_linktorsrc
Discipline Engineering
EISSN 1557-9603
EndPage 4389
ExternalDocumentID 10_1109_TAES_2021_3103237
9512490
Genre orig-research
GrantInformation_xml – fundername: Natural Science Foundation of Hebei Province
  grantid: F2020203105; F2017203130
  funderid: 10.13039/501100003787
– fundername: National Natural Science Foundation of China
  grantid: 61673294
  funderid: 10.13039/501100001809
GroupedDBID -~X
0R~
29I
4.4
41~
5GY
5VS
6IK
97E
AAJGR
AARMG
AASAJ
AAWTH
ABAZT
ABQJQ
ABVLG
ACGFO
ACIWK
ACNCT
AENEX
AETIX
AGQYO
AGSQL
AHBIQ
AI.
AIBXA
AKJIK
AKQYR
ALLEH
ALMA_UNASSIGNED_HOLDINGS
ASUFR
ATWAV
BEFXN
BFFAM
BGNUA
BKEBE
BPEOZ
CS3
DU5
EBS
EJD
F5P
H~9
IAAWW
IBMZZ
ICLAB
IFIPE
IFJZH
IPLJI
JAVBF
LAI
M43
OCL
P2P
RIA
RIE
RNS
TN5
VH1
AAYOK
AAYXX
CITATION
RIG
7SP
7TB
8FD
FR3
H8D
L7M
ID FETCH-LOGICAL-c293t-43e258c8ebc7bd9819e842cbf9b81c3b46fdc1fe0c7ee6e90b63041da7d9b8143
IEDL.DBID RIE
ISSN 0018-9251
IngestDate Mon Jun 30 10:20:03 EDT 2025
Tue Jul 01 00:48:33 EDT 2025
Thu Apr 24 22:57:04 EDT 2025
Wed Aug 27 05:11:52 EDT 2025
IsPeerReviewed true
IsScholarly true
Issue 6
Language English
License https://ieeexplore.ieee.org/Xplorehelp/downloads/license-information/IEEE.html
LinkModel DirectLink
MergedId FETCHMERGED-LOGICAL-c293t-43e258c8ebc7bd9819e842cbf9b81c3b46fdc1fe0c7ee6e90b63041da7d9b8143
Notes ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 14
ORCID 0000-0001-9740-4367
0000-0003-0734-6728
0000-0002-8180-7839
0000-0001-6311-2112
PQID 2605706266
PQPubID 85477
PageCount 15
ParticipantIDs crossref_primary_10_1109_TAES_2021_3103237
proquest_journals_2605706266
ieee_primary_9512490
crossref_citationtrail_10_1109_TAES_2021_3103237
ProviderPackageCode CITATION
AAYXX
PublicationCentury 2000
PublicationDate 2021-12-01
PublicationDateYYYYMMDD 2021-12-01
PublicationDate_xml – month: 12
  year: 2021
  text: 2021-12-01
  day: 01
PublicationDecade 2020
PublicationPlace New York
PublicationPlace_xml – name: New York
PublicationTitle IEEE transactions on aerospace and electronic systems
PublicationTitleAbbrev T-AES
PublicationYear 2021
Publisher IEEE
The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher_xml – name: IEEE
– name: The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
References ref57
ref13
ref12
ref59
ref58
ref14
ref53
ref52
ref55
ref11
ref54
ref10
ref17
ref16
ref19
ref18
ref51
ref50
ref46
ref45
ref48
ref47
ref41
gao (ref49) 2021; 51
keshmniri (ref3) 0
zhang (ref40) 2017; 46
ref8
ref7
ref9
ref4
ref6
ref5
ref35
ref34
ref37
ref36
ref31
ref30
ref33
ref32
fiorentini (ref56) 0
ref2
ref39
ref38
ref24
ref23
ref26
ref25
ref20
levin (ref43) 0
ref22
ge (ref42) 2011
ref21
ref28
ref27
ref29
shaughnessy (ref1) 1990
ref60
yang (ref44) 2016
ref61
ding (ref15) 2020
References_xml – ident: ref41
  doi: 10.2514/6.2010-8285
– ident: ref53
  doi: 10.1007/s11071-017-3824-3
– ident: ref17
  doi: 10.3724/SP.J.1004.2013.01901
– ident: ref21
  doi: 10.1002/acs.2664
– ident: ref51
  doi: 10.1109/TAC.2011.2160030
– year: 0
  ident: ref3
  article-title: Six-DOF modeling and simulation of a generic hypersonic vehicle for control and navigation purposes
  publication-title: Proc AIAA Guid Navig Control Conf Exhibit
– ident: ref36
  doi: 10.1109/TASE.2020.3008846
– year: 0
  ident: ref43
  article-title: Adaptive mode suppression scheme for an aeroelastic air-breathing hypersonic cruise vehicle
  publication-title: Proc AIAA Guid Navig Control Conf Exhibit
– year: 1990
  ident: ref1
  article-title: Hypersonic vehicle simulation model: Winged-cone configuration
– year: 2016
  ident: ref44
  article-title: Nonlinear robust control for cruise tracking of air breathing hypersonic vehicle
– ident: ref35
  doi: 10.1109/TII.2019.2914478
– ident: ref27
  doi: 10.1049/iet-cta.2016.1256
– ident: ref7
  doi: 10.2514/1.G002777
– ident: ref47
  doi: 10.1109/TFUZZ.2019.2934934
– ident: ref22
  doi: 10.1109/TAES.2020.3040519
– ident: ref11
  doi: 10.2514/1.23370
– ident: ref8
  doi: 10.2514/1.J054428
– ident: ref45
  doi: 10.2514/1.57739
– ident: ref29
  doi: 10.1016/j.ins.2019.08.012
– ident: ref19
  doi: 10.1109/TSMC.2018.2847706
– ident: ref50
  doi: 10.1109/ACC.2009.5160211
– volume: 46
  start-page: 90
  year: 2017
  ident: ref40
  article-title: A survey of models and control problems of hypersonic vehicles
  publication-title: Inf Control
– ident: ref13
  doi: 10.2514/1.27830
– ident: ref5
  doi: 10.2514/6.2009-5601
– ident: ref14
  doi: 10.2514/1.39210
– ident: ref30
  doi: 10.1109/TAC.2011.2179869
– ident: ref16
  doi: 10.2514/6.2003-7081
– ident: ref55
  doi: 10.1016/j.actaastro.2019.07.041
– ident: ref48
  doi: 10.1016/j.ast.2021.106554
– ident: ref52
  doi: 10.1109/TIE.2013.2271597
– ident: ref24
  doi: 10.1016/j.isatra.2018.12.043
– ident: ref10
  doi: 10.2514/3.21349
– ident: ref12
  doi: 10.2514/6.2007-6396
– ident: ref20
  doi: 10.1109/TII.2019.2945861
– ident: ref54
  doi: 10.1049/iet-cta.2016.1457
– volume: 51
  start-page: 1981
  year: 2021
  ident: ref49
  article-title: Interval type-2 FNN-based quantized tracking control for hypersonic flight vehicles with prescribed performance
  publication-title: IEEE Trans Syst Man Cybern Syst
– year: 2020
  ident: ref15
  article-title: Research on finite-time control methods of air-breathing hypersonic vehicle
– ident: ref26
  doi: 10.1109/TIE.2015.2442224
– ident: ref28
  doi: 10.1109/TIE.2017.2739700
– year: 2011
  ident: ref42
  article-title: Robust gain-scheduling control of hypersonic vehicle in near space
– ident: ref32
  doi: 10.1016/j.automatica.2015.01.021
– ident: ref18
  doi: 10.1109/TSMC.2018.2837378
– ident: ref9
  doi: 10.2514/6.2016-1325
– ident: ref34
  doi: 10.1109/TAC.2021.3053194
– ident: ref46
  doi: 10.1109/TAES.2020.2999149
– year: 0
  ident: ref56
  article-title: Nonlinear robust/adaptive controller design for an airbreathing hypersonic vehicle model
  publication-title: Proc AIAA Guid Navig Control Conf Exhibit
– ident: ref31
  doi: 10.1109/TAC.2016.2600343
– ident: ref57
  doi: 10.1109/CDC.2008.4739001
– ident: ref58
  doi: 10.1016/j.ast.2019.105608
– ident: ref6
  doi: 10.2514/6.2011-6227
– ident: ref25
  doi: 10.1016/j.jfranklin.2018.01.042
– ident: ref37
  doi: 10.1109/TCST.2016.2603072
– ident: ref2
  doi: 10.2514/6.2004-4805
– ident: ref33
  doi: 10.1080/00207179.2016.1207101
– ident: ref4
  doi: 10.2514/6.2007-6626
– ident: ref60
  doi: 10.1109/TCYB.2018.2794972
– ident: ref61
  doi: 10.1049/iet-cta.2018.5482
– ident: ref39
  doi: 10.1016/j.neucom.2015.08.017
– ident: ref59
  doi: 10.1109/TAC.2021.3059689
– ident: ref23
  doi: 10.1109/TIE.2017.2701776
– ident: ref38
  doi: 10.1109/ACCESS.2019.2900252
SSID ssj0014843
Score 2.4579294
Snippet This article addresses the tracking control problem of a hypersonic vehicle subject to multisource uncertainty and actuator fault. A composite fixed time...
SourceID proquest
crossref
ieee
SourceType Aggregation Database
Enrichment Source
Index Database
Publisher
StartPage 4375
SubjectTerms Actuators
Aerodynamics
Altitude
Atmospheric modeling
Control systems design
Controllers
Disturbance observers
Fast fixed time filter (FFTF)
fixed-time disturbance observer (FTDO)
hypersonic vehicle (HSV)
Hypersonic vehicles
Mathematical model
nonsingular fast terminal sliding mode controller
practically fixed time control
Sliding mode control
Stability
Stability analysis
Subsystems
Tracking control
Tracking errors
Uncertainty
Vehicle dynamics
Title Composite Practically Fixed Time Controller Design for a Hypersonic Vehicle With Multisource Uncertainty and Actuator Fault
URI https://ieeexplore.ieee.org/document/9512490
https://www.proquest.com/docview/2605706266
Volume 57
hasFullText 1
inHoldings 1
isFullTextHit
isPrint
link http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwjV1LT8MwDI6AExx4I8ZLPnBCdPSRvo4TME1IcIEBt6pJHDExbQg6icefx067CQFC3Hpw2kh2Yn_1Z1uIQ2tyX0eh9TKKRz3y19ZTUhqy5TxRJkhtUjJQvLxKen15cR_fz4njWS0MIjryGbb50eXyzVhP-FfZCUUDhBYIoM8TcKtrtWYZA5k1DLmADjA57SaDGfj5yU3n_JqQYBi0eahWyCPPv_ggN1Tlx03s3Et3RVxON1azSh7bk0q19fu3no3_3fmqWG7iTOjUhrEm5nC0Lpa-dB_cEB98FzBnC6HuWkTqGr5Bd_CKBrg0BE5rHvsQn-HMMT2AQlwooUfglQP1gYZbfOAPwN2gegBXzVunA6BP1uTYBtUblCMDHa5UIYAP3ZKkNkW_e35z2vOaWQyepoCg8mSEYZzpDJVOlckpjsBMhlrZXGWBjpRMrNGBRV-niAnmvkoiXwamTA1LyGhLLIzGI9wWEJZxiTGijWOUgWvBpm2GqYpNmCtZtoQ_1U6hm0blPC9jWDjA4ucFK7RghRaNQlviaLbkqe7S8ZfwBitoJtjopiX2piZQNOf4pWC0l_oE-pKd31ftikV-d01w2RML1fME9ylMqdSBs89PGHHlkw
linkProvider IEEE
linkToHtml http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwjV1LTxsxEB4heqA99EUrArSdQ09VN-zD-zpGlChQwqVJy221tsciahQQbCSgf74z3k2E2qritoexbGnGnu_beQF8dLYMTRK7oGA8GrC_doFWyrItl5m2Ue6yWoji-CwbTdXJeXq-AZ_XtTBE5JPPqC-fPpZvL81SfpUdMBpgtsAE_Qn7_TRuq7XWMQNVdDlyEV9hdttdDDMKy4PJ4Ogbc8E46stYrViGnj_wQn6syl9vsXcwwxcwXh2tzSv52V82um_u_-ja-Nizv4TnHdLEQWsar2CDFq_h2YP-g9vwS14DydoibPsWscLmdzic3ZJFKQ7BwzaTfU7X-MXneiCDXKxxxPRVoPrM4He6kA3wx6y5QF_P2wYEcMr25PMNmjusFxYHUqvCFB-HNUu9genwaHI4CrppDIFhSNAEKqE4LUxB2uTalowkqFCx0a7URWQSrTJnTeQoNDlRRmWosyRUka1zKxIqeQubi8sF7QDGdVpTSuTSlFTkm7AZV1CuUxuXWtU9CFfaqUzXqlwmZswrT1nCshKFVqLQqlNoDz6tl1y1fTr-J7wtCloLdrrpwf7KBKruJt9UwvfykGlftvvvVR9gazQZn1anx2df9-Cp7NOmu-zDZnO9pHcMWhr93tvqbzlU6N0
openUrl ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Ajournal&rft.genre=article&rft.atitle=Composite+Practically+Fixed+Time+Controller+Design+for+a+Hypersonic+Vehicle+With+Multisource+Uncertainty+and+Actuator+Fault&rft.jtitle=IEEE+transactions+on+aerospace+and+electronic+systems&rft.au=Wang%2C+Fang&rft.au=Li%2C+Yaping&rft.au=Zhou%2C+Chao&rft.au=Zong%2C+Qun&rft.date=2021-12-01&rft.issn=0018-9251&rft.eissn=1557-9603&rft.volume=57&rft.issue=6&rft.spage=4375&rft.epage=4389&rft_id=info:doi/10.1109%2FTAES.2021.3103237&rft.externalDBID=n%2Fa&rft.externalDocID=10_1109_TAES_2021_3103237
thumbnail_l http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=0018-9251&client=summon
thumbnail_m http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=0018-9251&client=summon
thumbnail_s http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=0018-9251&client=summon