{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2024,7,30]],"date-time":"2024-07-30T05:48:34Z","timestamp":1722318514798},"reference-count":29,"publisher":"Institute of Electrical and Electronics Engineers (IEEE)","license":[{"start":{"date-parts":[[2022,1,1]],"date-time":"2022-01-01T00:00:00Z","timestamp":1640995200000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/ieeexplore.ieee.org\/Xplorehelp\/downloads\/license-information\/IEEE.html"},{"start":{"date-parts":[[2022,1,1]],"date-time":"2022-01-01T00:00:00Z","timestamp":1640995200000},"content-version":"stm-asf","delay-in-days":0,"URL":"https:\/\/doi.org\/10.15223\/policy-029"},{"start":{"date-parts":[[2022,1,1]],"date-time":"2022-01-01T00:00:00Z","timestamp":1640995200000},"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":[[2022]]},"DOI":"10.1109\/taes.2022.3198033","type":"journal-article","created":{"date-parts":[[2022,8,10]],"date-time":"2022-08-10T19:32:58Z","timestamp":1660159978000},"page":"1-16","source":"Crossref","is-referenced-by-count":3,"title":["Minimum-time Trajectory Generation of eVTOL in Low-Speed Phase: Application in Control Law Design"],"prefix":"10.1109","author":[{"ORCID":"http:\/\/orcid.org\/0000-0002-2882-0583","authenticated-orcid":false,"given":"Mingkai","family":"Wang","sequence":"first","affiliation":[{"name":"School of Transportation Science and Engineering, Beihang University, Beijing, China"}]},{"given":"Nana","family":"Chu","sequence":"additional","affiliation":[{"name":"School of Transportation Science and Engineering, Beihang University, Beijing, China"}]},{"given":"Pranav","family":"Bhardwaj","sequence":"additional","affiliation":[{"name":"Institute of Flight System Dynamics, Technical University of Munich, Munich, Bavaria, Germany"}]},{"ORCID":"http:\/\/orcid.org\/0000-0003-2959-6197","authenticated-orcid":false,"given":"Shuguang","family":"Zhang","sequence":"additional","affiliation":[{"name":"School of Transportation Science and Engineering, Beihang University, Beijing, China"}]},{"ORCID":"http:\/\/orcid.org\/0000-0003-4733-9186","authenticated-orcid":false,"given":"Florian","family":"Holzapfel","sequence":"additional","affiliation":[{"name":"Institute of Flight System Dynamics, Technical University of Munich, Munich, Bavaria, Germany"}]}],"member":"263","reference":[{"key":"ref1","article-title":"Are air taxis ready for prime time?","author":"Schunck","year":"2021"},{"key":"ref2","doi-asserted-by":"publisher","DOI":"10.2514\/1.C035218"},{"key":"ref3","doi-asserted-by":"publisher","DOI":"10.1016\/j.cja.2020.04.021"},{"key":"ref4","first-page":"1","article-title":"Multidisciplinary systems analysis of a six passenger quadrotor urban air mobility vehicle powertrain","volume-title":"Proc. AIAA\/IEEE Elect. Aircr. Technol. Symp.","author":"Thomas","year":"2020"},{"key":"ref5","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2021.106903"},{"key":"ref6","article-title":"Handling qualities requirements and control design for high-speed rotorcraft","author":"Berger","year":"2019"},{"key":"ref7","article-title":"Aeronautical design standard performance specification handling qualities requirements for military rotorcraft","author":"Baskett","year":"2000"},{"key":"ref8","doi-asserted-by":"publisher","DOI":"10.1109\/TAES.2018.2890375"},{"key":"ref9","doi-asserted-by":"publisher","DOI":"10.2514\/6.2021-0577"},{"key":"ref10","doi-asserted-by":"publisher","DOI":"10.1137\/1.9780898718577.ch4"},{"key":"ref11","doi-asserted-by":"publisher","DOI":"10.2514\/3.21080"},{"key":"ref12","doi-asserted-by":"publisher","DOI":"10.2514\/6.2006-6598"},{"key":"ref13","doi-asserted-by":"publisher","DOI":"10.1002\/9781119971191.ch2"},{"key":"ref14","doi-asserted-by":"publisher","DOI":"10.1002\/oca.2347"},{"key":"ref15","doi-asserted-by":"publisher","DOI":"10.2307\/2372560"},{"key":"ref16","doi-asserted-by":"publisher","DOI":"10.2140\/pjm.1990.145.367"},{"key":"ref17","doi-asserted-by":"publisher","DOI":"10.1109\/TAES.2018.2811158"},{"key":"ref18","doi-asserted-by":"publisher","DOI":"10.1007\/s10514-012-9282-3"},{"key":"ref19","doi-asserted-by":"publisher","DOI":"10.1016\/j.automatica.2020.109240"},{"key":"ref20","doi-asserted-by":"publisher","DOI":"10.1016\/S0021-8928(00)00076-9"},{"key":"ref21","doi-asserted-by":"publisher","DOI":"10.1137\/0315023"},{"key":"ref22","article-title":"FALCON.m user guide","author":"Rieck"},{"key":"ref23","doi-asserted-by":"publisher","DOI":"10.1145\/2558904"},{"key":"ref24","doi-asserted-by":"publisher","DOI":"10.2514\/6.2018-3478"},{"key":"ref25","doi-asserted-by":"publisher","DOI":"10.2514\/6.2018-3479.c1"},{"key":"ref26","doi-asserted-by":"publisher","DOI":"10.2514\/1.G004520"},{"key":"ref27","article-title":"Flying qualities of piloted airplanes","year":"2006"},{"key":"ref28","doi-asserted-by":"publisher","DOI":"10.2514\/6.2002-6018"},{"key":"ref29","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2020.106126"}],"container-title":["IEEE Transactions on Aerospace and Electronic Systems"],"original-title":[],"link":[{"URL":"http:\/\/xplorestaging.ieee.org\/ielx7\/7\/7778228\/09854125.pdf?arnumber=9854125","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2024,2,1]],"date-time":"2024-02-01T12:08:33Z","timestamp":1706789313000},"score":1,"resource":{"primary":{"URL":"https:\/\/ieeexplore.ieee.org\/document\/9854125\/"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2022]]},"references-count":29,"URL":"https:\/\/doi.org\/10.1109\/taes.2022.3198033","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":[[2022]]}}}