{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,5,13]],"date-time":"2026-05-13T06:14:34Z","timestamp":1778652874844,"version":"3.51.4"},"reference-count":31,"publisher":"Institute of Electrical and Electronics Engineers (IEEE)","license":[{"start":{"date-parts":[[2020,1,1]],"date-time":"2020-01-01T00:00:00Z","timestamp":1577836800000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/creativecommons.org\/licenses\/by\/4.0\/legalcode"}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":["IEEE Access"],"published-print":{"date-parts":[[2020]]},"DOI":"10.1109\/access.2020.2977535","type":"journal-article","created":{"date-parts":[[2020,3,4]],"date-time":"2020-03-04T21:17:27Z","timestamp":1583356647000},"page":"43736-43751","source":"Crossref","is-referenced-by-count":11,"title":["A Multivariate Optimal Control Strategy for the Attitude Tracking of a Parafoil-UAV System"],"prefix":"10.1109","volume":"8","author":[{"ORCID":"https:\/\/orcid.org\/0000-0003-4329-1605","authenticated-orcid":false,"given":"Feikai","family":"Lv","sequence":"first","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]},{"ORCID":"https:\/\/orcid.org\/0000-0003-0410-9444","authenticated-orcid":false,"given":"Weiliang","family":"He","sequence":"additional","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]},{"ORCID":"https:\/\/orcid.org\/0000-0003-1384-4117","authenticated-orcid":false,"given":"Linggong","family":"Zhao","sequence":"additional","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]}],"member":"263","reference":[{"key":"ref31","first-page":"196","article-title":"Aircraft dynamic derivatives calculation using CFD techniques","volume":"39","author":"ye","year":"2013","journal-title":"J Beijing Univ Aeronaut Astronaut"},{"key":"ref30","doi-asserted-by":"publisher","DOI":"10.2514\/6.2016-1536"},{"key":"ref10","doi-asserted-by":"publisher","DOI":"10.1109\/ACCESS.2019.2943496"},{"key":"ref11","doi-asserted-by":"publisher","DOI":"10.1002\/0471669784"},{"key":"ref12","doi-asserted-by":"publisher","DOI":"10.1016\/j.isatra.2016.02.024"},{"key":"ref13","doi-asserted-by":"publisher","DOI":"10.1109\/TCST.2012.2229465"},{"key":"ref14","doi-asserted-by":"publisher","DOI":"10.1016\/j.enbuild.2014.11.036"},{"key":"ref15","doi-asserted-by":"publisher","DOI":"10.1109\/87.826801"},{"key":"ref16","doi-asserted-by":"publisher","DOI":"10.1016\/j.jfranklin.2017.02.033"},{"key":"ref17","doi-asserted-by":"publisher","DOI":"10.1016\/j.enconman.2017.03.072"},{"key":"ref18","doi-asserted-by":"publisher","DOI":"10.1109\/TMECH.2017.2766882"},{"key":"ref19","first-page":"2120","article-title":"A high-fidelity nonlinear multibody simulation model for parafoil systems","author":"m\u00fcller","year":"2012","journal-title":"Proc 16th AIAA Aerodyn Decelerator Syst Technol Conf Seminar"},{"key":"ref28","doi-asserted-by":"publisher","DOI":"10.1016\/j.automatica.2012.05.059"},{"key":"ref4","doi-asserted-by":"publisher","DOI":"10.1109\/TENCON.2013.6719061"},{"key":"ref27","doi-asserted-by":"publisher","DOI":"10.1016\/j.mcm.2006.02.015"},{"key":"ref3","doi-asserted-by":"publisher","DOI":"10.2514\/2.2854"},{"key":"ref6","doi-asserted-by":"publisher","DOI":"10.1177\/0954410017751815"},{"key":"ref29","doi-asserted-by":"publisher","DOI":"10.1016\/j.apm.2018.12.006"},{"key":"ref5","doi-asserted-by":"publisher","DOI":"10.1080\/00207721.2018.1433245"},{"key":"ref8","doi-asserted-by":"publisher","DOI":"10.2514\/1.25074"},{"key":"ref7","first-page":"6795","article-title":"Dynamics of a UAV with parafoil under powered flight","author":"wise","year":"2012","journal-title":"Proc AIAA Guid Navigat Control Conf Exhibit"},{"key":"ref2","first-page":"1497","article-title":"Precision parafoil recovery&#x2014;Providing flexibility for battlefield UAV systems?","author":"wyllie","year":"2012","journal-title":"Proc 14th AIAA Aerodynamic Decelerator Systems Technology Conf"},{"key":"ref9","first-page":"1857","article-title":"Improved digital model of parafoil-unmanned aerial vehicle accurate recycling system","author":"li","year":"2016","journal-title":"Proc IEEE Chin Guid Navigat Control Conf (CGNCC)"},{"key":"ref1","doi-asserted-by":"publisher","DOI":"10.1108\/00022660110696696"},{"key":"ref20","doi-asserted-by":"publisher","DOI":"10.2514\/2.6933"},{"key":"ref22","first-page":"1236","article-title":"Apparent mass effects on parafoil dynamics","author":"lissaman","year":"2012","journal-title":"Proc Aerospace Conf"},{"key":"ref21","doi-asserted-by":"publisher","DOI":"10.2514\/4.101960"},{"key":"ref24","first-page":"108","author":"stevens","year":"2016","journal-title":"Aircraft Control and Simulation"},{"key":"ref23","doi-asserted-by":"publisher","DOI":"10.2514\/2.2949"},{"key":"ref26","doi-asserted-by":"publisher","DOI":"10.2514\/1.G001545"},{"key":"ref25","first-page":"2768","article-title":"Modeling and Hardware-in-the-Loop simulation for a small unmanned aerial vehicle","author":"jung","year":"2012","journal-title":"Proc AIAA Infotech Aerospace Conf Exhibit"}],"container-title":["IEEE Access"],"original-title":[],"link":[{"URL":"http:\/\/xplorestaging.ieee.org\/ielx7\/6287639\/8948470\/09023946.pdf?arnumber=9023946","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2022,1,12]],"date-time":"2022-01-12T01:08:13Z","timestamp":1641949693000},"score":1,"resource":{"primary":{"URL":"https:\/\/ieeexplore.ieee.org\/document\/9023946\/"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2020]]},"references-count":31,"URL":"https:\/\/doi.org\/10.1109\/access.2020.2977535","relation":{},"ISSN":["2169-3536"],"issn-type":[{"value":"2169-3536","type":"electronic"}],"subject":[],"published":{"date-parts":[[2020]]}}}