{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2024,9,20]],"date-time":"2024-09-20T16:51:10Z","timestamp":1726851070184},"reference-count":41,"publisher":"Institute of Electrical and Electronics Engineers (IEEE)","license":[{"start":{"date-parts":[[2021,1,1]],"date-time":"2021-01-01T00:00:00Z","timestamp":1609459200000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/creativecommons.org\/licenses\/by-nc-nd\/4.0\/"},{"start":{"date-parts":[[2021,1,1]],"date-time":"2021-01-01T00:00:00Z","timestamp":1609459200000},"content-version":"am","delay-in-days":0,"URL":"https:\/\/creativecommons.org\/licenses\/by-nc-nd\/4.0\/"}],"funder":[{"DOI":"10.13039\/501100019271","name":"Foundation of Beijing Advanced Discipline Center for Unmanned Aircraft System, Beijing, China","doi-asserted-by":"publisher","id":[{"id":"10.13039\/501100019271","id-type":"DOI","asserted-by":"publisher"}]}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":["IEEE Access"],"published-print":{"date-parts":[[2021]]},"DOI":"10.1109\/access.2021.3131565","type":"journal-article","created":{"date-parts":[[2021,11,30]],"date-time":"2021-11-30T23:36:50Z","timestamp":1638315410000},"page":"161141-161160","source":"Crossref","is-referenced-by-count":4,"title":["Preliminary Design Method and Prototype Testing of a Novel Rotors Retractable Hybrid VTOL UAV"],"prefix":"10.1109","volume":"9","author":[{"ORCID":"http:\/\/orcid.org\/0000-0003-2540-897X","authenticated-orcid":false,"given":"Zijian","family":"Xiong","sequence":"first","affiliation":[]},{"ORCID":"http:\/\/orcid.org\/0000-0001-6759-1851","authenticated-orcid":false,"given":"Yuanming","family":"Xu","sequence":"additional","affiliation":[]},{"ORCID":"http:\/\/orcid.org\/0000-0002-5573-826X","authenticated-orcid":false,"given":"Zhouyang","family":"Wang","sequence":"additional","affiliation":[]},{"ORCID":"http:\/\/orcid.org\/0000-0002-6851-1523","authenticated-orcid":false,"given":"Xuechao","family":"Pian","sequence":"additional","affiliation":[]},{"ORCID":"http:\/\/orcid.org\/0000-0002-1524-1064","authenticated-orcid":false,"given":"Yibing","family":"Wang","sequence":"additional","affiliation":[]}],"member":"263","reference":[{"key":"ref39","first-page":"1339","article-title":"Modeling and experiment of power system for electric UAV","volume":"24","author":"chen","year":"2009","journal-title":"J Aerosp Power"},{"key":"ref38","author":"tu","year":"2012","journal-title":"Computational Fluid Dynamics A Practical Approach"},{"key":"ref33","doi-asserted-by":"publisher","DOI":"10.1109\/TMECH.2019.2890901"},{"key":"ref32","year":"2021","journal-title":"Flight Evalution"},{"key":"ref31","year":"2021","journal-title":"eCalc Solution for All Markus Müller"},{"key":"ref30","doi-asserted-by":"publisher","DOI":"10.1109\/TIE.2018.2885715"},{"key":"ref37","author":"fang","year":"2005","journal-title":"Aircraft Flight Dynamics"},{"key":"ref36","author":"cook","year":"2012","journal-title":"Flight Dynamics Principles A Linear Systems Approach to Aircraft Stability and Control"},{"key":"ref35","first-page":"260","article-title":"Modelling and performance impact of high power\/high energy battery hybrids on fixed-wing eVTOL UAV","author":"stahl","year":"2020","journal-title":"Proc AIAA SciTech Forum"},{"key":"ref34","doi-asserted-by":"publisher","DOI":"10.1016\/j.paerosci.2006.04.001"},{"key":"ref10","year":"2021","journal-title":"DoAero DA-EX6 VTOL UAV"},{"key":"ref40","first-page":"1","article-title":"Configuration redesign and prototype flight testing of an unmanned fixed-wing eVTOL aircraft with under-fuselage hover lift and pusher wingtip propulsion system","author":"stahl","year":"2019","journal-title":"Proc 8th Biennial Auton VTOL Tech Meeting 6th Annu Electr VTOL Symp"},{"key":"ref11","doi-asserted-by":"publisher","DOI":"10.2514\/4.104909"},{"key":"ref12","doi-asserted-by":"publisher","DOI":"10.2514\/4.868443"},{"key":"ref13","doi-asserted-by":"publisher","DOI":"10.1007\/978-90-481-9707-1"},{"key":"ref14","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2017.09.008"},{"key":"ref15","doi-asserted-by":"publisher","DOI":"10.1002\/9781119406303"},{"key":"ref16","year":"2021","journal-title":"ALTI Company"},{"key":"ref17","year":"2021","journal-title":"Sparkle Tech"},{"key":"ref18","year":"2021","journal-title":"EWATT Offical Site"},{"key":"ref19","year":"2021","journal-title":"Instrutial VTOL UAV"},{"key":"ref28","doi-asserted-by":"publisher","DOI":"10.2514\/6.2016-0581"},{"key":"ref4","doi-asserted-by":"publisher","DOI":"10.1016\/j.comcom.2019.10.016"},{"key":"ref27","doi-asserted-by":"publisher","DOI":"10.1007\/978-981-15-3138-5"},{"key":"ref3","author":"hirschberg","year":"2006","journal-title":"An Overview of the History of Vertical and\/or Short take-off and Landing (v\/stol) Aircraft"},{"key":"ref6","doi-asserted-by":"publisher","DOI":"10.3390\/aerospace6030026"},{"key":"ref29","doi-asserted-by":"publisher","DOI":"10.1109\/TMECH.2017.2675913"},{"key":"ref5","author":"mccormick","year":"1999","journal-title":"Aerodynamics of V\/STOL Flight"},{"key":"ref8","author":"eshel","year":"2021","journal-title":"Hybrid Quadrotor Debut at AUVSI"},{"key":"ref7","first-page":"1","article-title":"Development and performance comparison of optimized electric fixed-wing VTOL UAV configurations","author":"stahl","year":"2018","journal-title":"Proc 31st Congr Int Council Aeronaut Sci"},{"key":"ref2","doi-asserted-by":"publisher","DOI":"10.2514\/6.1990-3236"},{"key":"ref9","author":"kipp","year":"2021","journal-title":"Krossblade Skyprowler"},{"key":"ref1","first-page":"127","article-title":"Development and trend analysis of VTOL aircraft (in Chinese)","volume":"6","author":"liu","year":"2015","journal-title":"Advances in Aeronautical Science and Engineering"},{"key":"ref20","doi-asserted-by":"publisher","DOI":"10.1002\/9781118352700"},{"key":"ref22","doi-asserted-by":"publisher","DOI":"10.2200\/S00789ED1V01Y201707MEC004"},{"key":"ref21","doi-asserted-by":"publisher","DOI":"10.1016\/S1369-8869(00)00012-4"},{"key":"ref24","doi-asserted-by":"publisher","DOI":"10.1007\/978-3-642-84010-4_1"},{"key":"ref41","author":"brescianini","year":"2013","journal-title":"Nonlinear quadrocopter attitude control technical report"},{"key":"ref23","doi-asserted-by":"publisher","DOI":"10.1002\/9781118454190"},{"key":"ref26","doi-asserted-by":"publisher","DOI":"10.1007\/978-981-10-3382-7"},{"key":"ref25","doi-asserted-by":"publisher","DOI":"10.2514\/4.862274"}],"container-title":["IEEE Access"],"original-title":[],"link":[{"URL":"http:\/\/xplorestaging.ieee.org\/ielx7\/6287639\/9312710\/09628104.pdf?arnumber=9628104","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2022,3,8]],"date-time":"2022-03-08T21:58:45Z","timestamp":1646776725000},"score":1,"resource":{"primary":{"URL":"https:\/\/ieeexplore.ieee.org\/document\/9628104\/"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2021]]},"references-count":41,"URL":"https:\/\/doi.org\/10.1109\/access.2021.3131565","relation":{},"ISSN":["2169-3536"],"issn-type":[{"value":"2169-3536","type":"electronic"}],"subject":[],"published":{"date-parts":[[2021]]}}}