{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,5,12]],"date-time":"2026-05-12T16:52:34Z","timestamp":1778604754646,"version":"3.51.4"},"reference-count":41,"publisher":"Institute of Electrical and Electronics Engineers (IEEE)","issue":"6","license":[{"start":{"date-parts":[[2024,12,1]],"date-time":"2024-12-01T00:00:00Z","timestamp":1733011200000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/ieeexplore.ieee.org\/Xplorehelp\/downloads\/license-information\/IEEE.html"},{"start":{"date-parts":[[2024,12,1]],"date-time":"2024-12-01T00:00:00Z","timestamp":1733011200000},"content-version":"stm-asf","delay-in-days":0,"URL":"https:\/\/doi.org\/10.15223\/policy-029"},{"start":{"date-parts":[[2024,12,1]],"date-time":"2024-12-01T00:00:00Z","timestamp":1733011200000},"content-version":"stm-asf","delay-in-days":0,"URL":"https:\/\/doi.org\/10.15223\/policy-037"}],"funder":[{"name":"Science Center for Gas Turbine","award":["P2022-B-V-002-001"],"award-info":[{"award-number":["P2022-B-V-002-001"]}]},{"name":"AECC Industry–University Research","award":["HFZL2022CXY006"],"award-info":[{"award-number":["HFZL2022CXY006"]}]}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":["IEEE Trans. Aerosp. Electron. Syst."],"published-print":{"date-parts":[[2024,12]]},"DOI":"10.1109\/taes.2024.3435631","type":"journal-article","created":{"date-parts":[[2024,7,30]],"date-time":"2024-07-30T18:08:44Z","timestamp":1722362924000},"page":"8929-8944","source":"Crossref","is-referenced-by-count":6,"title":["LSTM\u2013Fuzzy Logic for Fault Forecasting and Mitigation in Propulsion System"],"prefix":"10.1109","volume":"60","author":[{"ORCID":"https:\/\/orcid.org\/0009-0002-0308-357X","authenticated-orcid":false,"given":"Bingqiang","family":"Yu","sequence":"first","affiliation":[{"name":"College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China"}]},{"ORCID":"https:\/\/orcid.org\/0009-0001-8313-5052","authenticated-orcid":false,"given":"Yi","family":"Peng","sequence":"additional","affiliation":[{"name":"Shanghai Aerospace Control Technology Institute, China Aerospace Science and Technology Corporation, Shanghai, China"}]},{"given":"Jinquan","family":"Huang","sequence":"additional","affiliation":[{"name":"College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China"}]},{"ORCID":"https:\/\/orcid.org\/0000-0002-6620-2399","authenticated-orcid":false,"given":"Feng","family":"Lu","sequence":"additional","affiliation":[{"name":"College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China"}]}],"member":"263","reference":[{"issue":"5","key":"ref1","first-page":"6","article-title":"Mathematical modeling and simulation for steady state of a 75-ton liquid propellant rocket engine","volume":"11","author":"Lee","year":"2017","journal-title":"J. Aerosp. Syst. Eng."},{"key":"ref2","doi-asserted-by":"publisher","DOI":"10.15407\/itm2020.01.005"},{"key":"ref3","doi-asserted-by":"publisher","DOI":"10.2514\/6.2018-4602"},{"key":"ref4","doi-asserted-by":"publisher","DOI":"10.3390\/s24020415"},{"key":"ref5","doi-asserted-by":"publisher","DOI":"10.1016\/j.ijhydene.2017.06.242"},{"key":"ref6","doi-asserted-by":"publisher","DOI":"10.1016\/j.actaastro.2004.05.070"},{"key":"ref7","doi-asserted-by":"publisher","DOI":"10.2514\/2.5327"},{"key":"ref8","doi-asserted-by":"publisher","DOI":"10.2514\/6.2004-3514"},{"key":"ref9","doi-asserted-by":"publisher","DOI":"10.1109\/AERO.2011.5747596"},{"key":"ref10","doi-asserted-by":"publisher","DOI":"10.2514\/6.2009-4958"},{"key":"ref11","doi-asserted-by":"publisher","DOI":"10.2514\/1.42783"},{"key":"ref12","doi-asserted-by":"publisher","DOI":"10.1016\/j.actaastro.2020.08.019"},{"key":"ref13","article-title":"Critical measurement parameters estimation in liquid rocket engine using LSTM-based soft sensor","volume":"92","author":"Devakumar","year":"2023","journal-title":"Flow Meas. Instrum."},{"key":"ref14","doi-asserted-by":"publisher","DOI":"10.2514\/6.2021-3506"},{"key":"ref15","doi-asserted-by":"publisher","DOI":"10.1016\/j.actaastro.2019.03.075"},{"key":"ref16","doi-asserted-by":"publisher","DOI":"10.1109\/TIM.2021.3086900"},{"key":"ref17","doi-asserted-by":"publisher","DOI":"10.1016\/j.ress.2023.109837"},{"key":"ref18","doi-asserted-by":"publisher","DOI":"10.3390\/aerospace9090481"},{"key":"ref19","doi-asserted-by":"publisher","DOI":"10.3390\/s21155026"},{"issue":"6","key":"ref20","first-page":"90","article-title":"Thrust closed-loop control of the large scale expendable liquid rocket propulsion","volume":"27","author":"Xue","year":"2019","journal-title":"Comput. Meas. Control"},{"key":"ref21","first-page":"443","article-title":"Design and performance evaluation of a flow regulator for thrust control of a liquid rocket engine","volume-title":"Proc. Korean Soc. Propulsion Eng. Conf.","author":"Jung","year":"2012"},{"key":"ref22","doi-asserted-by":"publisher","DOI":"10.1016\/j.paerosci.2019.03.002"},{"key":"ref23","doi-asserted-by":"publisher","DOI":"10.1109\/ICMAE52228.2021.9522512"},{"key":"ref24","doi-asserted-by":"publisher","DOI":"10.3390\/aerospace10010032"},{"key":"ref25","doi-asserted-by":"publisher","DOI":"10.3390\/electronics10030285"},{"key":"ref26","doi-asserted-by":"publisher","DOI":"10.1162\/neco.1997.9.8.1735"},{"key":"ref27","doi-asserted-by":"publisher","DOI":"10.1016\/j.ress.2021.107807"},{"key":"ref28","doi-asserted-by":"publisher","DOI":"10.1109\/ACCESS.2020.2992044"},{"key":"ref29","doi-asserted-by":"publisher","DOI":"10.1162\/neco_a_01199"},{"key":"ref30","doi-asserted-by":"publisher","DOI":"10.1080\/01430750.2014.952844"},{"key":"ref31","doi-asserted-by":"publisher","DOI":"10.3991\/ijet.v14i11.10280"},{"key":"ref32","doi-asserted-by":"publisher","DOI":"10.1016\/j.psep.2021.12.015"},{"key":"ref33","doi-asserted-by":"publisher","DOI":"10.1115\/1.4047014"},{"key":"ref34","doi-asserted-by":"publisher","DOI":"10.1016\/j.eswa.2011.04.198"},{"issue":"S2","key":"ref35","first-page":"49","article-title":"Performance evaluation method for liquid rocket engine under malfunction","volume":"37","author":"Liang","year":"2020","journal-title":"Aerosp. Shanghai"},{"key":"ref36","doi-asserted-by":"publisher","DOI":"10.1177\/0954410016656878"},{"key":"ref37","doi-asserted-by":"publisher","DOI":"10.2514\/6.2024-0522"},{"key":"ref38","doi-asserted-by":"publisher","DOI":"10.1109\/TAES.2024.3350012"},{"key":"ref39","doi-asserted-by":"publisher","DOI":"10.1016\/j.engappai.2023.107114"},{"key":"ref40","doi-asserted-by":"publisher","DOI":"10.1109\/IETC57902.2023.10152188"},{"key":"ref41","doi-asserted-by":"publisher","DOI":"10.1016\/j.eswa.2021.115016"}],"container-title":["IEEE Transactions on Aerospace and Electronic Systems"],"original-title":[],"link":[{"URL":"http:\/\/xplorestaging.ieee.org\/ielx8\/7\/10779571\/10614857.pdf?arnumber=10614857","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2024,12,11]],"date-time":"2024-12-11T03:01:01Z","timestamp":1733886061000},"score":1,"resource":{"primary":{"URL":"https:\/\/ieeexplore.ieee.org\/document\/10614857\/"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2024,12]]},"references-count":41,"journal-issue":{"issue":"6"},"URL":"https:\/\/doi.org\/10.1109\/taes.2024.3435631","relation":{},"ISSN":["0018-9251","1557-9603","2371-9877"],"issn-type":[{"value":"0018-9251","type":"print"},{"value":"1557-9603","type":"electronic"},{"value":"2371-9877","type":"electronic"}],"subject":[],"published":{"date-parts":[[2024,12]]}}}