Tracking Controller Design for Satellite Attitude Under Unknown Constant Disturbance Using Stable Embedding
We propose a tracking control law for the fully actuated rigid body system in the presence of any unknown constant disturbance by employing quaternions with the stable embedding technique and Lyapunov stability theory. The stable embedding technique extends the attitude dynamics from the set of unit...
Saved in:
Published in | Journal of electrical engineering & technology Vol. 16; no. 2; pp. 1089 - 1097 |
---|---|
Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
Singapore
Springer Singapore
01.03.2021
Springer 대한전기학회 |
Subjects | |
Online Access | Get full text |
ISSN | 1975-0102 2093-7423 |
DOI | 10.1007/s42835-020-00622-3 |
Cover
Abstract | We propose a tracking control law for the fully actuated rigid body system in the presence of any unknown constant disturbance by employing quaternions with the stable embedding technique and Lyapunov stability theory. The stable embedding technique extends the attitude dynamics from the set of unit quaternions to the set of quaternions, which is a Euclidean space, such that the set of unit quaternions is an invariant set of the extended dynamics. Such a stable extension of the system dynamics to a Euclidean space allows us to employ well studied Lyapunov techniques in Euclidean spaces such as LaSalle–Yoshizawa’s theorem. A robust tracking control law is proposed for the attitude dynamics subject to unknown constant disturbance and the convergence properties of the tracking control law is rigorously proven. It is demonstrated with the help of numerical simulations that the proposed control law has a remarkable performance even in some challenging situations. |
---|---|
AbstractList | We propose a tracking control law for the fully actuated rigid body system in the presence of any unknown constant disturbance by employing quaternions with the stable embedding technique and Lyapunov stability theory. The stable embedding technique extends the attitude dynamics from the set of unit quaternions to the set of quaternions, which is a Euclidean space, such that the set of unit quaternions is an invariant set of the extended dynamics. Such a stable extension of the system dynamics to a Euclidean space allows us to employ well studied Lyapunov techniques in Euclidean spaces such as LaSalle–Yoshizawa’s theorem. A robust tracking control law is proposed for the attitude dynamics subject to unknown constant disturbance and the convergence properties of the tracking control law is rigorously proven. It is demonstrated with the help of numerical simulations that the proposed control law has a remarkable performance even in some challenging situations. We propose a tracking control law for the fully actuated rigid body system in the presence of any unknown constant disturbance by employing quaternions with the stable embedding technique and Lyapunov stability theory. The stable embedding technique extends the attitude dynamics from the set of unit quaternions to the set of quaternions, which is a Euclidean space, such that the set of unit quaternions is an invariant set of the extended dynamics. Such a stable extension of the system dynamics to a Euclidean space allows us to employ well studied Lyapunov techniques in Euclidean spaces such as LaSalle– Yoshizawa’s theorem. A robust tracking control law is proposed for the attitude dynamics subject to unknown constant disturbance and the convergence properties of the tracking control law is rigorously proven. It is demonstrated with the help of numerical simulations that the proposed control law has a remarkable performance even in some challenging situations. KCI Citation Count: 0 |
Author | Chang, Dong Eui Ko, Wonshick Phogat, Karmvir Singh Petit, Nicolas |
Author_xml | – sequence: 1 givenname: Wonshick surname: Ko fullname: Ko, Wonshick organization: Hanon Systems – sequence: 2 givenname: Karmvir Singh surname: Phogat fullname: Phogat, Karmvir Singh organization: Department of Mathematical Engineering and Information Physics, University of Tokyo – sequence: 3 givenname: Nicolas surname: Petit fullname: Petit, Nicolas organization: CAS, MINES ParisTech – sequence: 4 givenname: Dong Eui orcidid: 0000-0002-6496-4189 surname: Chang fullname: Chang, Dong Eui email: dechang@kaist.ac.kr organization: School of Electrical Engineering, Korea Advanced Institute of Science and Technology |
BackLink | https://minesparis-psl.hal.science/hal-03184384$$DView record in HAL https://www.kci.go.kr/kciportal/ci/sereArticleSearch/ciSereArtiView.kci?sereArticleSearchBean.artiId=ART002691725$$DAccess content in National Research Foundation of Korea (NRF) |
BookMark | eNp9kU1LAzEQhoMoWKt_wNNePaxOPrbZPZb6CQXBtueQzWZrumsiSar47822ouChhzAweZ5JmPcMHVtnNUKXGK4xAL8JjJS0yIFADjAhJKdHaESgojlnhB6jEa54usZATtFZCJsEYSjoCHVLL1Vn7DqbORu963vts1sdzNpmrfPZQkbd9ybqbBqjidtGZyvbJGZlO-s-7aCFKG3Mbk2IW19LqxIShomLKOteZ3dvtW6a1DhHJ63sg774qWO0ur9bzh7z-fPD02w6zxUtqpizgsgGNNW1AkIZkKpitGWV5owr1dZS4fT3pgCNOU6Hq6rlStYTWkgoJiUdo6v9XOtb0SkjnDS7unai82L6snwSFZ8AKdgf-yp78e7Nm_RfO_5xOhdDDyguGS3ZB04s2bPKuxC8bn8FDGKIQexjECkGsYtB0CSV_yRlooxm2LY0_WGV7tWQ3rFr7cXGbb1NqztkfQOGWZ3- |
CitedBy_id | crossref_primary_10_3390_s21165609 crossref_primary_10_1002_rnc_6514 crossref_primary_10_1109_TCST_2024_3351074 |
Cites_doi | 10.1002/rnc.4294 10.1109/TAC.2015.2407452 10.1016/j.automatica.2004.02.022 10.1007/s00332-016-9316-7 10.1016/j.ifacol.2017.08.1579 10.2514/1.G003566 10.1109/9.467669 10.1115/1.4041447 10.1016/j.sysconle.2011.10.017 |
ContentType | Journal Article |
Copyright | The Korean Institute of Electrical Engineers 2020 Distributed under a Creative Commons Attribution 4.0 International License |
Copyright_xml | – notice: The Korean Institute of Electrical Engineers 2020 – notice: Distributed under a Creative Commons Attribution 4.0 International License |
DBID | AAYXX CITATION 1XC ACYCR |
DOI | 10.1007/s42835-020-00622-3 |
DatabaseName | CrossRef Hyper Article en Ligne (HAL) Korean Citation Index |
DatabaseTitle | CrossRef |
DatabaseTitleList | |
DeliveryMethod | fulltext_linktorsrc |
Discipline | Engineering |
EISSN | 2093-7423 |
EndPage | 1097 |
ExternalDocumentID | oai_kci_go_kr_ARTI_9760254 oai_HAL_hal_03184384v1 10_1007_s42835_020_00622_3 |
GrantInformation_xml | – fundername: KAIST grantid: Engineering Global Initiative funderid: https://doi.org/10.13039/501100007107 |
GroupedDBID | -~X .UV 0R~ 2WC 406 9ZL AACDK AAHNG AAJBT AASML AATNV AAUYE AAYYP ABAKF ABECU ABFTV ABJNI ABKCH ABMQK ABTEG ABTKH ABTMW ACAOD ACDTI ACHSB ACOKC ACPIV ACZOJ ADKNI ADTPH ADURQ ADYFF AEFQL AEMSY AENEX AESKC AFBBN AFQWF AGDGC AGMZJ AGQEE AIGIU AILAN AITGF AJZVZ ALMA_UNASSIGNED_HOLDINGS AMKLP AMXSW AMYLF AXYYD BGNMA CSCUP DBRKI DPUIP EBLON EBS EJD FIGPU FNLPD FRJ GGCAI GW5 IKXTQ IWAJR JDI JZLTJ KOV KVFHK LLZTM M4Y NPVJJ NQJWS NU0 OK1 PT4 ROL RSV SJYHP SNE SNPRN SOHCF SOJ SRMVM SSLCW TDB UOJIU UTJUX VEKWB VFIZW ZMTXR AAYXX ABBRH ABDBE ABFSG ACSTC AEZWR AFDZB AFHIU AFOHR AHPBZ AHWEU AIXLP ATHPR AYFIA CITATION 1XC ACYCR |
ID | FETCH-LOGICAL-c359t-452ad0e3ebc0234029943f49e747ccfbac1105d50e171e177c9f7cab635a05683 |
ISSN | 1975-0102 |
IngestDate | Sun Mar 09 07:54:40 EDT 2025 Fri May 09 12:24:09 EDT 2025 Thu Apr 24 23:13:28 EDT 2025 Tue Jul 01 00:40:51 EDT 2025 Fri Feb 21 02:49:28 EST 2025 |
IsPeerReviewed | true |
IsScholarly | true |
Issue | 2 |
Keywords | Satellite Embedding Attitude tracking control Quaternions Lyapunov function |
Language | English |
License | Distributed under a Creative Commons Attribution 4.0 International License: http://creativecommons.org/licenses/by/4.0 |
LinkModel | OpenURL |
MergedId | FETCHMERGED-LOGICAL-c359t-452ad0e3ebc0234029943f49e747ccfbac1105d50e171e177c9f7cab635a05683 |
ORCID | 0000-0002-6496-4189 0000-0003-3581-3856 |
PageCount | 9 |
ParticipantIDs | nrf_kci_oai_kci_go_kr_ARTI_9760254 hal_primary_oai_HAL_hal_03184384v1 crossref_primary_10_1007_s42835_020_00622_3 crossref_citationtrail_10_1007_s42835_020_00622_3 springer_journals_10_1007_s42835_020_00622_3 |
ProviderPackageCode | CITATION AAYXX |
PublicationCentury | 2000 |
PublicationDate | 20210300 2021-03-00 2021-03 |
PublicationDateYYYYMMDD | 2021-03-01 |
PublicationDate_xml | – month: 3 year: 2021 text: 20210300 |
PublicationDecade | 2020 |
PublicationPlace | Singapore |
PublicationPlace_xml | – name: Singapore |
PublicationTitle | Journal of electrical engineering & technology |
PublicationTitleAbbrev | J. Electr. Eng. Technol |
PublicationYear | 2021 |
Publisher | Springer Singapore Springer 대한전기학회 |
Publisher_xml | – name: Springer Singapore – name: Springer – name: 대한전기학회 |
References | Chang (CR2) 2018; 28 Lovera, Astolfi (CR9) 2004; 40 Khalil (CR4) 2002 Joshi, Kelkar, Wen (CR3) 1995; 40 Xia, Su (CR12) 2018; 41 Lee (CR8) 2015; 60 CR5 Magnis, Petit (CR10) 2017; 50 Lee, Chang, Eun (CR7) 2019; 141 Chang, Jiménez, Perlmutter (CR1) 2016; 26 Lee (CR6) 2012; 61 Mayhew, Sanfelice, Teel (CR11) 2012; 56 HK Khalil (622_CR4) 2002 T Lee (622_CR6) 2012; 61 T Lee (622_CR8) 2015; 60 622_CR5 DE Chang (622_CR1) 2016; 26 DE Chang (622_CR2) 2018; 28 M Lovera (622_CR9) 2004; 40 Y Xia (622_CR12) 2018; 41 T Lee (622_CR7) 2019; 141 L Magnis (622_CR10) 2017; 50 CG Mayhew (622_CR11) 2012; 56 SM Joshi (622_CR3) 1995; 40 |
References_xml | – volume: 28 start-page: 4981 issue: 16 year: 2018 end-page: 4998 ident: CR2 article-title: On controller design for systems on manifolds in Euclidean space publication-title: Int J Robust Nonlinear Control doi: 10.1002/rnc.4294 – volume: 60 start-page: 2837 issue: 10 year: 2015 end-page: 2842 ident: CR8 article-title: Global exponential attitude tracking controls on SO(3) publication-title: IEEE Trans Autom Control doi: 10.1109/TAC.2015.2407452 – volume: 40 start-page: 1405 issue: 8 year: 2004 end-page: 1414 ident: CR9 article-title: Spacecraft attitude control using magnetic actuators publication-title: Automatica doi: 10.1016/j.automatica.2004.02.022 – volume: 56 start-page: 2146 issue: 11 year: 2012 end-page: 2152 ident: CR11 article-title: Quaternion-based hybrid control for robust global attitude tracking publication-title: IEEE Trans Autom Control – volume: 26 start-page: 1693 issue: 6 year: 2016 end-page: 1721 ident: CR1 article-title: Feedback integrators publication-title: J Nonlinear Sci doi: 10.1007/s00332-016-9316-7 – ident: CR5 – year: 2002 ident: CR4 publication-title: Nonlinear Syst – volume: 50 start-page: 9000 issue: 1 year: 2017 end-page: 9007 ident: CR10 article-title: Angular velocity and torque estimation from vector measurements publication-title: IFAC-PapersOnLine doi: 10.1016/j.ifacol.2017.08.1579 – volume: 41 start-page: 2298 issue: 10 year: 2018 end-page: 2305 ident: CR12 article-title: Saturated output feedback control for global asymptotic attitude tracking of spacecraft publication-title: J Guid Control Dyn doi: 10.2514/1.G003566 – volume: 40 start-page: 1800 issue: 10 year: 1995 end-page: 1803 ident: CR3 article-title: Robust attitude stabilization of spacecraft using nonlinear quaternion feedback publication-title: IEEE Trans Autom Control doi: 10.1109/9.467669 – volume: 141 start-page: 021005 year: 2019 ident: CR7 article-title: Semiglobal nonmemoryless attitude controls on the special orthogonal group publication-title: ASME J Dyn Syst Meas Control doi: 10.1115/1.4041447 – volume: 61 start-page: 231 issue: 1 year: 2012 end-page: 237 ident: CR6 article-title: Exponential stability of an attitude tracking control system on SO(3) for large-angle rotational maneuvers publication-title: Syst Control Lett doi: 10.1016/j.sysconle.2011.10.017 – volume: 61 start-page: 231 issue: 1 year: 2012 ident: 622_CR6 publication-title: Syst Control Lett doi: 10.1016/j.sysconle.2011.10.017 – volume: 40 start-page: 1800 issue: 10 year: 1995 ident: 622_CR3 publication-title: IEEE Trans Autom Control doi: 10.1109/9.467669 – volume: 28 start-page: 4981 issue: 16 year: 2018 ident: 622_CR2 publication-title: Int J Robust Nonlinear Control doi: 10.1002/rnc.4294 – ident: 622_CR5 – volume: 41 start-page: 2298 issue: 10 year: 2018 ident: 622_CR12 publication-title: J Guid Control Dyn doi: 10.2514/1.G003566 – volume: 50 start-page: 9000 issue: 1 year: 2017 ident: 622_CR10 publication-title: IFAC-PapersOnLine doi: 10.1016/j.ifacol.2017.08.1579 – volume-title: Nonlinear Syst year: 2002 ident: 622_CR4 – volume: 60 start-page: 2837 issue: 10 year: 2015 ident: 622_CR8 publication-title: IEEE Trans Autom Control doi: 10.1109/TAC.2015.2407452 – volume: 141 start-page: 021005 year: 2019 ident: 622_CR7 publication-title: ASME J Dyn Syst Meas Control doi: 10.1115/1.4041447 – volume: 40 start-page: 1405 issue: 8 year: 2004 ident: 622_CR9 publication-title: Automatica doi: 10.1016/j.automatica.2004.02.022 – volume: 56 start-page: 2146 issue: 11 year: 2012 ident: 622_CR11 publication-title: IEEE Trans Autom Control – volume: 26 start-page: 1693 issue: 6 year: 2016 ident: 622_CR1 publication-title: J Nonlinear Sci doi: 10.1007/s00332-016-9316-7 |
SSID | ssj0061053 |
Score | 2.2207417 |
Snippet | We propose a tracking control law for the fully actuated rigid body system in the presence of any unknown constant disturbance by employing quaternions with... |
SourceID | nrf hal crossref springer |
SourceType | Open Website Open Access Repository Enrichment Source Index Database Publisher |
StartPage | 1089 |
SubjectTerms | Automatic Electrical Engineering Electrical Machines and Networks Electronics and Microelectronics Engineering Engineering Sciences Instrumentation Original Article Power Electronics 전기공학 |
Title | Tracking Controller Design for Satellite Attitude Under Unknown Constant Disturbance Using Stable Embedding |
URI | https://link.springer.com/article/10.1007/s42835-020-00622-3 https://minesparis-psl.hal.science/hal-03184384 https://www.kci.go.kr/kciportal/ci/sereArticleSearch/ciSereArtiView.kci?sereArticleSearchBean.artiId=ART002691725 |
Volume | 16 |
hasFullText | 1 |
inHoldings | 1 |
isFullTextHit | |
isPrint | |
ispartofPNX | Journal of Electrical Engineering & Technology, 2021, 16(2), , pp.1089-1097 |
link | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwnV3fb9owELZo-7I9TPupsXWTNe2tyxQchySPaQuia4cqtWh9s2LHKYgWpjT0oX_n_qDdOYkTBKq6PRBQcOLg-zjfne8-E_KVgQugQ62dkCvmIKWbk8jId8JQc85YINMU4x0_x_3RhP-48q86nT-trKVVIb-rh611Jf8jVTgHcsUq2X-QrL0pnIDPIF84goTh-DQZ54malwv3JuH8RuegQDAlw2QPXiSGbrPQB3GBGQEpmpjIHTFZYCjNlPuhcVggBydMPdKUD5RJBGCEYk3V4Fbq1E5vm0ZsuYuOEbRumA0NnoqNoP2pCcv-MhliylYInU-X10lRFabd3s_gueEW00ZnQ6cWs4l1AY7qSPcx7pY0WM3a8QvWSuBai1-2dHAUYD6hWyppbc4xN_IcXFReU9z9FkBZSwv33HJbompGx0X2rbNFmSByZzjnHPSjsaKUOV4zN9b5AKP4QpwfD8XZyfh0_VvL0T2Kz8QUIIRaknshvweffI8FASYP7MXDw8NxbSGAxWrYUe0PrYq5TEnnxsOsGUw7U0zX3Vnk2cbKvTGILl-SFxUIaFzC8hXp6MVr8rzFb_mGzGuA0gagtAQoBYBSC1BaA5QagNIKoLQGKG0BlBqA0hKg1AL0LZkMB5dHI6fa3cNRnh8VDvdZkrra01KB3chdsIu4l_FIg4OrVCYTBZapn_qu7gU9eAUqygKVSLCQE7DaQ-8d2V0sF_o9oT54BUmo4ZLIR4ZJGWUZlyroB1ngKd3vkl49hEJV1Pe4A8uNsKTdZtgFDLswwy68Ljmw1_wuiV8ebf0FZV833I4HaASCE3M1Mw3w_Xop5rkA1_VEgF-AzBRd8q2Wq6hUzd0jHX94SscfybPmn7dPdot8pT-BLV3IzxU0_wKjnMdd |
linkProvider | Library Specific Holdings |
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=Tracking+Controller+Design+for+Satellite+Attitude+Under+Unknown+Constant+Disturbance+Using+Stable+Embedding&rft.jtitle=Journal+of+electrical+engineering+%26+technology&rft.au=Ko%2C+Wonshick&rft.au=Phogat%2C+Karmvir+Singh&rft.au=Petit%2C+Nicolas&rft.au=Chang%2C+Dong+Eui&rft.date=2021-03-01&rft.pub=Springer&rft.issn=1975-0102&rft.eissn=2093-7423&rft.volume=16&rft.issue=2&rft.spage=1089&rft.epage=1097&rft_id=info:doi/10.1007%2Fs42835-020-00622-3&rft.externalDBID=HAS_PDF_LINK&rft.externalDocID=oai_HAL_hal_03184384v1 |
thumbnail_l | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=1975-0102&client=summon |
thumbnail_m | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=1975-0102&client=summon |
thumbnail_s | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=1975-0102&client=summon |