{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,5,27]],"date-time":"2026-05-27T18:15:07Z","timestamp":1779905707164,"version":"3.53.1"},"reference-count":21,"publisher":"Institute of Electrical and Electronics Engineers (IEEE)","issue":"3","license":[{"start":{"date-parts":[[2024,6,1]],"date-time":"2024-06-01T00:00:00Z","timestamp":1717200000000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/ieeexplore.ieee.org\/Xplorehelp\/downloads\/license-information\/IEEE.html"},{"start":{"date-parts":[[2024,6,1]],"date-time":"2024-06-01T00:00:00Z","timestamp":1717200000000},"content-version":"stm-asf","delay-in-days":0,"URL":"https:\/\/doi.org\/10.15223\/policy-029"},{"start":{"date-parts":[[2024,6,1]],"date-time":"2024-06-01T00:00:00Z","timestamp":1717200000000},"content-version":"stm-asf","delay-in-days":0,"URL":"https:\/\/doi.org\/10.15223\/policy-037"}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":["IEEE Trans. Aerosp. Electron. Syst."],"published-print":{"date-parts":[[2024,6]]},"DOI":"10.1109\/taes.2024.3358263","type":"journal-article","created":{"date-parts":[[2024,1,24]],"date-time":"2024-01-24T18:43:38Z","timestamp":1706121818000},"page":"3121-3131","source":"Crossref","is-referenced-by-count":7,"title":["A Comprehensive Model of Variable Pitch Electric Propulsion Unit for Optimal-Power Thrust Control"],"prefix":"10.1109","volume":"60","author":[{"ORCID":"https:\/\/orcid.org\/0000-0003-0453-087X","authenticated-orcid":false,"given":"Jiaxin","family":"Wu","sequence":"first","affiliation":[{"name":"Department of Electrical Engineering, Harbin Institute of Technology, Harbin, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"ORCID":"https:\/\/orcid.org\/0000-0003-4743-0860","authenticated-orcid":false,"given":"Yong","family":"Li","sequence":"additional","affiliation":[{"name":"Department of Electrical Engineering, Harbin Institute of Technology, Harbin, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"ORCID":"https:\/\/orcid.org\/0000-0002-5688-4269","authenticated-orcid":false,"given":"Jianhui","family":"Hu","sequence":"additional","affiliation":[{"name":"Department of Electrical Engineering, Harbin Institute of Technology, Harbin, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Chengjun","family":"Liu","sequence":"additional","affiliation":[{"name":"Department of Electrical Engineering, Harbin Institute of Technology, Harbin, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Meng","family":"Zhao","sequence":"additional","affiliation":[{"name":"Department of Electrical Engineering, Harbin Institute of Technology, Harbin, China"}],"role":[{"vocabulary":"crossref","role":"author"}]}],"member":"263","reference":[{"key":"ref1","doi-asserted-by":"publisher","DOI":"10.1109\/taes.2021.3082712"},{"key":"ref2","doi-asserted-by":"publisher","DOI":"10.1109\/tte.2022.3197332"},{"key":"ref3","doi-asserted-by":"publisher","DOI":"10.1109\/taes.2022.3198033"},{"key":"ref4","doi-asserted-by":"publisher","DOI":"10.1109\/TTE.2021.3068724"},{"key":"ref5","doi-asserted-by":"publisher","DOI":"10.1109\/tte.2015.2426499"},{"key":"ref6","doi-asserted-by":"publisher","DOI":"10.1109\/TAES.2012.6237610"},{"key":"ref7","doi-asserted-by":"publisher","DOI":"10.1007\/s10846-015-0311-2"},{"key":"ref8","doi-asserted-by":"publisher","DOI":"10.1115\/1.4030676"},{"key":"ref9","doi-asserted-by":"publisher","DOI":"10.1109\/CCA.2014.6981426"},{"key":"ref10","doi-asserted-by":"publisher","DOI":"10.1109\/ICCA.2018.8444363"},{"key":"ref11","doi-asserted-by":"publisher","DOI":"10.1109\/ICRA40945.2020.9197208"},{"key":"ref12","doi-asserted-by":"publisher","DOI":"10.1109\/PESGM.2018.8586666"},{"key":"ref13","first-page":"60","article-title":"Blade element analysis","volume-title":"Principles of Helicopter Aerodynamics","author":"Leishman","year":"2006"},{"key":"ref14","doi-asserted-by":"publisher","DOI":"10.1109\/ACCESS.2018.2879636"},{"key":"ref15","doi-asserted-by":"publisher","DOI":"10.1109\/TIA.2017.2740278"},{"key":"ref16","article-title":"Effect of a rapid blade-pitch increase on the thrust and induced-velocity response of a full-scale helicopter rotor","author":"Carpenter","year":"1953"},{"issue":"2","key":"ref17","article-title":"Analysis of power density and prospects of future technology requirement of permanent magnet motors used in aircraft","volume":"26","author":"Li","year":"2022","journal-title":"Electr. Mach. Control"},{"key":"ref18","doi-asserted-by":"publisher","DOI":"10.3390\/en9040232"},{"key":"ref19","doi-asserted-by":"publisher","DOI":"10.4050\/JAHS.15.31"},{"key":"ref20","doi-asserted-by":"publisher","DOI":"10.2514\/1.C031271"},{"key":"ref21","doi-asserted-by":"publisher","DOI":"10.4050\/JAHS.67.042006"}],"container-title":["IEEE Transactions on Aerospace and Electronic Systems"],"original-title":[],"link":[{"URL":"http:\/\/xplorestaging.ieee.org\/ielx7\/7\/10552647\/10413566.pdf?arnumber=10413566","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2024,6,25]],"date-time":"2024-06-25T21:05:40Z","timestamp":1719349540000},"score":1,"resource":{"primary":{"URL":"https:\/\/ieeexplore.ieee.org\/document\/10413566\/"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2024,6]]},"references-count":21,"journal-issue":{"issue":"3"},"URL":"https:\/\/doi.org\/10.1109\/taes.2024.3358263","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":[[2024,6]]}}}