Response Analysis of Projectile System Under Gaussian Noise Excitation Using Path Integral Method

During flight, projectiles are subject to uncertainties such as aerodynamic forces, wind gusts, and measurement errors; all of which significantly affect their stability and accuracy. As a result, studying the response of projectile systems under stochastic excitation is essential. This paper focuse...

Full description

Saved in:
Bibliographic Details
Published inInternational Journal of Aerospace Engineering Vol. 2024; no. 1
Main Authors Wang, Liang, Li, Xinyi, Peng, Jiahui, Zhang, Zhonghua, Dong, Shuangqi
Format Journal Article
LanguageEnglish
Published New York John Wiley & Sons, Inc 02.12.2024
Wiley
Subjects
Online AccessGet full text

Cover

Loading…
Abstract During flight, projectiles are subject to uncertainties such as aerodynamic forces, wind gusts, and measurement errors; all of which significantly affect their stability and accuracy. As a result, studying the response of projectile systems under stochastic excitation is essential. This paper focuses on the solution and analysis of projectile system responses under stochastic excitation. We employed the path integral method to compute the transient and stationary probability density functions for projectile systems subjected to Gaussian stochastic external and parametric excitations. Based on the probabilistic responses, we analyzed the evolution of the system’s probability density function over time under Gaussian white noise excitation, as well as the changes in the stationary probability density function with air density and flight speed as bifurcation parameters. The analysis results indicate that within a specific range of parameter variations, air density can induce stochastic P‐bifurcation phenomena. Furthermore, increasing air density and flight speed can enhance the stability of the projectile.
AbstractList During flight, projectiles are subject to uncertainties such as aerodynamic forces, wind gusts, and measurement errors; all of which significantly affect their stability and accuracy. As a result, studying the response of projectile systems under stochastic excitation is essential. This paper focuses on the solution and analysis of projectile system responses under stochastic excitation. We employed the path integral method to compute the transient and stationary probability density functions for projectile systems subjected to Gaussian stochastic external and parametric excitations. Based on the probabilistic responses, we analyzed the evolution of the system’s probability density function over time under Gaussian white noise excitation, as well as the changes in the stationary probability density function with air density and flight speed as bifurcation parameters. The analysis results indicate that within a specific range of parameter variations, air density can induce stochastic P‐bifurcation phenomena. Furthermore, increasing air density and flight speed can enhance the stability of the projectile.
Audience Academic
Author Peng, Jiahui
Dong, Shuangqi
Zhang, Zhonghua
Wang, Liang
Li, Xinyi
Author_xml – sequence: 1
  givenname: Liang
  surname: Wang
  fullname: Wang, Liang
– sequence: 2
  givenname: Xinyi
  orcidid: 0009-0008-2521-0350
  surname: Li
  fullname: Li, Xinyi
– sequence: 3
  givenname: Jiahui
  orcidid: 0009-0008-1532-125X
  surname: Peng
  fullname: Peng, Jiahui
– sequence: 4
  givenname: Zhonghua
  orcidid: 0009-0000-1641-3334
  surname: Zhang
  fullname: Zhang, Zhonghua
– sequence: 5
  givenname: Shuangqi
  orcidid: 0009-0009-0641-1752
  surname: Dong
  fullname: Dong, Shuangqi
BookMark eNptklFLHDEUhQexULW-9QcEfCp0NZnJTCaPi1i7YFXUfQ53Mjdjhtlkm2TB_ffNdkW6UPJwQ_jOgZx7Totj5x0WxVdGLxmr6ys7Al4JUdKGlUfFCWtaMaul4Mcf96b5XJzGOFLa0FrUJwU8YVx7F5HMHUzbaCPxhjwGP6JOdkLyvI0JV2TpegzkFjYxWnDk3tssuXnTNkGy3pFltG4gj5BeycIlHAJM5BemV99_KT4ZmCKev8-zYvnj5uX65-zu4XZxPb-baV6KNJPMiLoTdQNt38oGRUvLtuy7CrgWRkqhGTO05EY3FCouetNxg5IL0ZWUMazOisXet_cwqnWwKwhb5cGqvw8-DApCsnpCxU2JrKEtallxbljLmYGOljIbmYpV2eti77UO_vcGY1Kj34QcUFQV41ywmst_qAGyqXXGpwB6ZaNW85ZJWVMq20xd_ofKp8eV1XmBJsd8KPh2IMhMwrc07LJXi-enQ_b7ntXBxxjQfHycUbXrhNp1Qr13ovoDGRSoRw
Cites_doi 10.1103/PhysRevA.35.1795
10.1016/S0020-7462(96)00096-0
10.1016/j.ijnonlinmec.2023.104504
10.2514/3.25343
10.1016/j.ymssp.2012.02.013
10.1016/j.taml.2022.100385
10.2514/3.50025
10.1016/S0266-8920(99)00031-4
10.1016/j.jsv.2023.118037
10.1007/s11071-019-05159-3
10.1007/s11071-014-1310-8
10.1103/PhysRevA.28.3003
10.1016/j.strusafe.2015.11.001
10.21236/AD0442757
10.1007/s11071-016-3323-y
10.1016/0096-3003(90)90003-L
10.1007/s00707-013-1040-x
10.1016/j.ast.2016.10.016
10.2514/1.A33864
ContentType Journal Article
Copyright COPYRIGHT 2024 John Wiley & Sons, Inc.
Copyright © 2024 Liang Wang et al. This is an open access article distributed under the Creative Commons Attribution License (the “License”), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License. https://creativecommons.org/licenses/by/4.0
Copyright_xml – notice: COPYRIGHT 2024 John Wiley & Sons, Inc.
– notice: Copyright © 2024 Liang Wang et al. This is an open access article distributed under the Creative Commons Attribution License (the “License”), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License. https://creativecommons.org/licenses/by/4.0
DBID AAYXX
CITATION
ISR
7TB
8FD
8FE
8FG
ABJCF
ABUWG
AFKRA
ARAPS
AZQEC
BENPR
BGLVJ
CCPQU
CWDGH
DWQXO
FR3
H8D
HCIFZ
L6V
L7M
M7S
P5Z
P62
PHGZM
PHGZT
PIMPY
PKEHL
PQEST
PQGLB
PQQKQ
PQUKI
PRINS
PTHSS
DOA
DOI 10.1155/ijae/7720612
DatabaseName CrossRef
Gale In Context: Science
Mechanical & Transportation Engineering Abstracts
Technology Research Database
ProQuest SciTech Collection
ProQuest Technology Collection
SciTech Premium Collection
ProQuest Central (Alumni)
ProQuest Central UK/Ireland
Advanced Technologies & Aerospace Collection
ProQuest Central Essentials
ProQuest Central
Technology Collection
ProQuest One Community College
Middle East & Africa Database
ProQuest Central Korea
Engineering Research Database
Aerospace Database
SciTech Premium Collection
ProQuest Engineering Collection
Advanced Technologies Database with Aerospace
Engineering Database
Advanced Technologies & Aerospace Database
ProQuest Advanced Technologies & Aerospace Collection
ProQuest Central Premium
ProQuest One Academic
Publicly Available Content Database
ProQuest One Academic Middle East (New)
ProQuest One Academic Eastern Edition (DO NOT USE)
ProQuest One Applied & Life Sciences
ProQuest One Academic
ProQuest One Academic UKI Edition
ProQuest Central China
Engineering Collection
DOAJ Directory of Open Access Journals
DatabaseTitle CrossRef
Publicly Available Content Database
Technology Collection
Technology Research Database
ProQuest One Academic Middle East (New)
Mechanical & Transportation Engineering Abstracts
ProQuest Advanced Technologies & Aerospace Collection
ProQuest Central Essentials
ProQuest Central (Alumni Edition)
SciTech Premium Collection
ProQuest One Community College
ProQuest Central China
ProQuest Central
ProQuest One Applied & Life Sciences
Aerospace Database
ProQuest Engineering Collection
Middle East & Africa Database
ProQuest Central Korea
ProQuest Central (New)
Advanced Technologies Database with Aerospace
Engineering Collection
Advanced Technologies & Aerospace Collection
Engineering Database
ProQuest One Academic Eastern Edition
ProQuest Technology Collection
ProQuest SciTech Collection
Advanced Technologies & Aerospace Database
ProQuest One Academic UKI Edition
Materials Science & Engineering Collection
Engineering Research Database
ProQuest One Academic
ProQuest One Academic (New)
DatabaseTitleList CrossRef


Database_xml – sequence: 1
  dbid: DOA
  name: DOAJ Directory of Open Access Journals
  url: https://www.doaj.org/
  sourceTypes: Open Website
– sequence: 2
  dbid: 8FG
  name: ProQuest Technology Collection
  url: https://search.proquest.com/technologycollection1
  sourceTypes: Aggregation Database
DeliveryMethod fulltext_linktorsrc
Discipline Engineering
EISSN 1687-5974
Editor Tuo Han
Editor_xml – fullname: Tuo Han
ExternalDocumentID oai_doaj_org_article_4f2e1608ec9344f1841fab029011f313
A819950098
10_1155_ijae_7720612
GroupedDBID 0R~
188
24P
29J
2UF
2WC
4.4
5GY
5VS
8FE
8FG
8R4
8R5
AAFWJ
AAJEY
AAYXX
ABDBF
ABJCF
ABUWG
ACCMX
ACIWK
ACUHS
ADBBV
ADMLS
AEGXH
AENEX
AFKRA
AFPKN
AINHJ
ALMA_UNASSIGNED_HOLDINGS
ARAPS
BCNDV
BENPR
BGLVJ
BPHCQ
C1A
CCPQU
CITATION
CS3
CWDGH
E3Z
EBS
EJD
ESX
GROUPED_DOAJ
H13
HCIFZ
I-F
IAO
IEA
IL9
ISR
ITC
KQ8
L6V
M7S
MK~
OK1
OVT
P62
PHGZM
PHGZT
PIMPY
PQQKQ
PROAC
PTHSS
Q2X
RHU
RNS
TR2
TUS
UGNYK
UNMZH
~8M
M~E
7TB
8FD
AAMMB
AEFGJ
AGXDD
AIDQK
AIDYY
AZQEC
DWQXO
FR3
H8D
L7M
PKEHL
PQEST
PQGLB
PQUKI
PRINS
PUEGO
ID FETCH-LOGICAL-c427t-91f75b756a8d896e780282db3a4c7f997c11f024fc60a347dfb4fe9477b2011e3
IEDL.DBID BENPR
ISSN 1687-5966
IngestDate Wed Aug 27 01:30:54 EDT 2025
Fri Jul 25 19:01:32 EDT 2025
Thu Apr 17 06:54:43 EDT 2025
Tue Apr 15 04:04:16 EDT 2025
Fri Apr 11 03:21:33 EDT 2025
Tue Jul 01 02:40:18 EDT 2025
IsDoiOpenAccess true
IsOpenAccess true
IsPeerReviewed true
IsScholarly true
Issue 1
Language English
LinkModel DirectLink
MergedId FETCHMERGED-LOGICAL-c427t-91f75b756a8d896e780282db3a4c7f997c11f024fc60a347dfb4fe9477b2011e3
Notes ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 14
ORCID 0009-0009-0641-1752
0009-0008-1532-125X
0009-0000-1641-3334
0009-0008-2521-0350
OpenAccessLink https://www.proquest.com/docview/3144715493?pq-origsite=%requestingapplication%
PQID 3144715493
PQPubID 237291
ParticipantIDs doaj_primary_oai_doaj_org_article_4f2e1608ec9344f1841fab029011f313
proquest_journals_3144715493
gale_infotracmisc_A819950098
gale_infotracacademiconefile_A819950098
gale_incontextgauss_ISR_A819950098
crossref_primary_10_1155_ijae_7720612
ProviderPackageCode CITATION
AAYXX
PublicationCentury 2000
PublicationDate 2024-12-02
PublicationDateYYYYMMDD 2024-12-02
PublicationDate_xml – month: 12
  year: 2024
  text: 2024-12-02
  day: 02
PublicationDecade 2020
PublicationPlace New York
PublicationPlace_xml – name: New York
PublicationTitle International Journal of Aerospace Engineering
PublicationYear 2024
Publisher John Wiley & Sons, Inc
Wiley
Publisher_xml – name: John Wiley & Sons, Inc
– name: Wiley
References e_1_2_8_16_2
e_1_2_8_17_2
e_1_2_8_18_2
e_1_2_8_19_2
e_1_2_8_12_2
e_1_2_8_23_2
e_1_2_8_13_2
e_1_2_8_24_2
e_1_2_8_14_2
e_1_2_8_15_2
Zhong Y. W. (e_1_2_8_8_2) 2015; 36
e_1_2_8_9_2
Zhong Y. W. (e_1_2_8_7_2) 2015; 27
e_1_2_8_2_2
e_1_2_8_1_2
Ren T. R. (e_1_2_8_4_2) 2010; 31
e_1_2_8_6_2
e_1_2_8_5_2
e_1_2_8_20_2
e_1_2_8_10_2
e_1_2_8_21_2
e_1_2_8_11_2
Nicolaides J. D. (e_1_2_8_3_2) 1953; 395
Reeves P. M. (e_1_2_8_22_2) 1974
References_xml – ident: e_1_2_8_16_2
  doi: 10.1103/PhysRevA.35.1795
– ident: e_1_2_8_10_2
  doi: 10.1016/S0020-7462(96)00096-0
– ident: e_1_2_8_20_2
  doi: 10.1016/j.ijnonlinmec.2023.104504
– volume: 31
  start-page: 2082
  year: 2010
  ident: e_1_2_8_4_2
  article-title: Coning motion analysis of spinning missile based on gyrodynamics
  publication-title: Journal of Astronautics
– volume: 27
  year: 2015
  ident: e_1_2_8_7_2
  article-title: Stability analysis of periodic solutions for nonlinear angle motion of projectiles and rockets
  publication-title: Journal of Ballistics
– ident: e_1_2_8_23_2
  doi: 10.2514/3.25343
– ident: e_1_2_8_18_2
  doi: 10.1016/j.ymssp.2012.02.013
– ident: e_1_2_8_11_2
  doi: 10.1016/j.taml.2022.100385
– ident: e_1_2_8_2_2
  doi: 10.2514/3.50025
– ident: e_1_2_8_17_2
  doi: 10.1016/S0266-8920(99)00031-4
– ident: e_1_2_8_19_2
  doi: 10.1016/j.jsv.2023.118037
– volume: 395
  year: 1953
  ident: e_1_2_8_3_2
  article-title: On the free flight motion of missiles having slight configurational asymmetries
  publication-title: Institute of the Aeronautical Sciences
– volume: 36
  start-page: 1195
  year: 2015
  ident: e_1_2_8_8_2
  article-title: Hopf bifurcation analysis of nonlinear angular motion stability of projectile
  publication-title: Acta Armamentarii
– volume-title: Development and application of a non-Gaussian atmospheric turbulence model for use in flight simulators, NASA Contractor Report NASA CR-2451
  year: 1974
  ident: e_1_2_8_22_2
– ident: e_1_2_8_6_2
  doi: 10.1007/s11071-019-05159-3
– ident: e_1_2_8_12_2
  doi: 10.1007/s11071-014-1310-8
– ident: e_1_2_8_15_2
  doi: 10.1103/PhysRevA.28.3003
– ident: e_1_2_8_24_2
  doi: 10.1016/j.strusafe.2015.11.001
– ident: e_1_2_8_1_2
  doi: 10.21236/AD0442757
– ident: e_1_2_8_13_2
  doi: 10.1007/s11071-016-3323-y
– ident: e_1_2_8_21_2
  doi: 10.1016/0096-3003(90)90003-L
– ident: e_1_2_8_14_2
  doi: 10.1007/s00707-013-1040-x
– ident: e_1_2_8_5_2
  doi: 10.1016/j.ast.2016.10.016
– ident: e_1_2_8_9_2
  doi: 10.2514/1.A33864
SSID ssj0060575
ssib005317291
Score 2.2963476
Snippet During flight, projectiles are subject to uncertainties such as aerodynamic forces, wind gusts, and measurement errors; all of which significantly affect their...
SourceID doaj
proquest
gale
crossref
SourceType Open Website
Aggregation Database
Index Database
SubjectTerms Coordinate transformations
Distribution (Probability theory)
Methods
Projectiles
Random noise
Systems stability
Velocity
SummonAdditionalLinks – databaseName: DOAJ Directory of Open Access Journals
  dbid: DOA
  link: http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwrV1NTxsxELUqTvSACm1FaEBW1aqnVeL11_oICEgqgaK0SNws27ERCCUVSSR-PjP2LiIHxKXX3bG0frPjmdmdeUPID69mOrDAK6cYJCiM8apRw6aKioUUGojANfY7X16p0bX4fSNvXo36wpqwQg9cgBuIVEcGq2MwXIgECQlLzg_x9x9LPM-rrcHndclUOYMVRiFdmbuUg7t7FwcQR6I_33BAmaf_rdM4u5jzT2SnjQ3pcXmmXfIhzvfIx1eMgZ-Jm5aa1kg7NhG6SHRSPqeAgdPCQE7zOCN64dZLbJKkV4s7WHL2FFpGbporBegEwj86LoQRD_QyD5P-Qq7Pz_6ejqp2SkIVRK1XcFolLb2WyjWzxqioG0yjZp47EXQyBlTBEnjiFNTQcYA-eZGiEVp7dP6RfyVb88U87hNqAGljvBGzUAudlJMhgHuXUccEYZfvkZ8ddPZfIcOwOYmQ0iLEtoW4R04Q1xcZpLDOF0CxtlWsfU-xPfIdtWKRpGKOVTC3iJkd_5na4wYby5EKtUd-tUJpsXp0wbVNBbAf5LXakOxvSIIVhc3bnfJta8VLyyHb1Mhhxw_-x46-ke0aFJGLYeo-2Vo9ruMhhDQrf5Tf3me7v_FC
  priority: 102
  providerName: Directory of Open Access Journals
Title Response Analysis of Projectile System Under Gaussian Noise Excitation Using Path Integral Method
URI https://www.proquest.com/docview/3144715493
https://doaj.org/article/4f2e1608ec9344f1841fab029011f313
Volume 2024
hasFullText 1
inHoldings 1
isFullTextHit
isPrint
link http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV3db9MwELdY9wIPiE9RGJWFQDxFreP4I09oG_0YUquqMLE3y3HsaRNqRttJPPG3c-c4Y32Al0SKHUW5s8-_O59_R8j7StbKMcczKxk4KIzxTMuRzrxkLjgNCFzheef5Qs7Oiy8X4iIF3LYprbKzidFQ143DGPmQA_JXyCfGP938zLBqFO6uphIaB-QQTLDWPXJ4Ml4sV_dHGKDHu6QPiegEXTAJU0sA0u9S4YUYXl1bPwSsiWv-3iIVufz_ZbHjMjR5Qh4n_EiPW4U_JQ_8-hl5dI9V8Dmxqzbv1dOOcYQ2gS7bkAsYAdqylNNY8ohO7e0WD1LSRXMFr4x_ucTaTWM2AV0CRKRnLanEDzqPBadfkPPJ-NvpLEuVFDJX5GoHFi0oUSkhra51Kb3S6GrVFbeFU6EsQV0swGodnBxZDuoJVRF8WShVIUDw_CXprZu1f0Vo6Zksy6osapcXKkgrnAMIILzyAaBZ1ScfOtGZm5Yww0RHQwiDIjZJxH1ygnK964M01_FBs7k0adaYIuTwuZH2ruRFEcAbZcFWI9z7ZYEz3ifvUCsGiSzWmClziTIzZ19X5ljj4XOkS-2Tj6lTaHYb62w6eAD_g9xXez2P9nrCTHP7zZ3yTZrpW_N3XL7-f_Mb8jAHEcdUmPyI9HabW_8WAM2uGpADPZkO0tiF--n3z9PZIIYH4Dr_Pf4DyGD1Yw
linkProvider ProQuest
linkToHtml http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwtV1LbxMxELZKOQAHxFMECliIitMq8fq1PiBUoGlCm6gqrdSb8XrtqghlS5IK-FP9jZ3x7pbmALde197X2OP5xp75hpC3paq0Z55nTjFwUBjjWaEGRRYU89EXgMA15jtPpmp0JL4cy-M1ctHlwmBYZbcmpoW6qj3ukfc5IH-NfGL8w9nPDKtG4elqV0KjmRa74c8vcNkW78efYXw383y4ffhplLVVBTIvcr0E7Y5alloqV1SFUUEX6HZUJXfC62gMfDqLYLmiVwPH4VNjKWIwQusSjWXg8Nxb5LbgYMkxM324c30-A1a9CjFRiIXQ4VOgyBL8ii7wXsr-6XcX-oBsEWGsmMRUOeBf9iEZveEDcr9Fq3SrmV4PyVqYPSL3rnEYPibuoImyDbTjN6F1pPvNBg8sObThRKepwBLdcecLTNuk0_oUbtn-7VuOcJpiF-g-AFI6bigsftBJKm_9hBzdiISfkvVZPQvPCDWBKWNKIyqfCx2Vk94D4JBBhwhAsOyRzU509qyh57DJrZHSoohtK-Ie-YhyveqDpNrpQj0_sa2OWhFzeN2gCN5wISL4viy6coAnzSxyxnvkDY6KRdqMGcblnKDM7Pjrgd0qMNUdyVl75F3bKdbLufOuTXOA_0GmrZWeGys9Qa_9anM3-LZdVxb2rxY8_3_za3JndDjZs3vj6e4LcjcHcacgnHyDrC_n5-ElQKll-SrNX0q-3bTCXAK9wiuK
linkToPdf http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwtV1LbxMxEB6VVEJwQDxFoICFqDitEq9fuweEWprQUBpFgUq9Ga9jV0UoW5JUwF_rr-vMPkpzgFuvu97XeMbzjXfmG4A3hZ4Zz71InOYYoHAukkz3syRo7qPPEIEbqnc-HOv9I_npWB1vwEVbC0Nple2aWC3Us9LTHnlPIPI3xCcmerFJi5jsDd-f_UyogxT9aW3badQqchD-_MLwbflutIdzvZ2mw8HXD_tJ02Eg8TI1K7T0aFRhlHbZLMt1MBmFILNCOOlNzHP8DB7Ri0Wv-07ga8dCxpBLYwpynEHgfW_BpqGoqAObu4PxZHpduxG5XiWcaEJGFP5pNGuFUUabhq9U7_S7Cz3EuYQ31hxk1UfgX96icoHD-3Cvwa5sp1a2B7AR5g_h7jVGw0fgpnXObWAt2wkrI5vU2z24ALGaIZ1V7ZbYR3e-pCJONi5P8ZLBb98whrMqk4FNEJ6yUU1o8YMdVs2uH8PRjcj4CXTm5Tw8BZYHrvO8yOXMp9JE7ZT3CD9UMCEiLCy6sN2Kzp7VZB22CnKUsiRi24i4C7sk16sxRLFdHSgXJ7axWCtjio_rZ8HnQsqIkTCPrujTf2ceBRddeE2zYolEY07qeEIys6MvU7uTUeE7UbV24W0zKJarhfOuKXrA7yHerbWRW2sj0cr9-ul28m2zyiztX5t49v_Tr-A2Gov9PBofPIc7KUq7yshJt6CzWpyHF4irVsXLRoEZfLtpm7kE5x8xHA
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=Response+Analysis+of+Projectile+System+Under+Gaussian+Noise+Excitation+Using+Path+Integral+Method&rft.jtitle=International+journal+of+aerospace+engineering&rft.au=Wang%2C+Liang&rft.au=Li%2C+Xinyi&rft.au=Peng%2C+Jiahui&rft.au=Zhang%2C+Zhonghua&rft.date=2024-12-02&rft.pub=John+Wiley+%26+Sons%2C+Inc&rft.issn=1687-5966&rft.eissn=1687-5974&rft.volume=2024&rft_id=info:doi/10.1155%2Fijae%2F7720612&rft.externalDBID=HAS_PDF_LINK
thumbnail_l http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=1687-5966&client=summon
thumbnail_m http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=1687-5966&client=summon
thumbnail_s http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=1687-5966&client=summon