{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,6,26]],"date-time":"2026-06-26T14:07:33Z","timestamp":1782482853420,"version":"3.54.5"},"reference-count":33,"publisher":"Institute of Electrical and Electronics Engineers (IEEE)","issue":"1","license":[{"start":{"date-parts":[[2019,2,1]],"date-time":"2019-02-01T00:00:00Z","timestamp":1548979200000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/ieeexplore.ieee.org\/Xplorehelp\/downloads\/license-information\/IEEE.html"},{"start":{"date-parts":[[2019,2,1]],"date-time":"2019-02-01T00:00:00Z","timestamp":1548979200000},"content-version":"stm-asf","delay-in-days":0,"URL":"https:\/\/doi.org\/10.15223\/policy-029"},{"start":{"date-parts":[[2019,2,1]],"date-time":"2019-02-01T00:00:00Z","timestamp":1548979200000},"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":[[2019,2]]},"DOI":"10.1109\/taes.2018.2852369","type":"journal-article","created":{"date-parts":[[2018,7,2]],"date-time":"2018-07-02T18:48:01Z","timestamp":1530557281000},"page":"384-396","source":"Crossref","is-referenced-by-count":69,"title":["Disturbance Observer-Based Attitude Control for Spacecraft With Input MRS"],"prefix":"10.1109","volume":"55","author":[{"ORCID":"https:\/\/orcid.org\/0000-0001-8504-1677","authenticated-orcid":false,"given":"An-Min","family":"Zou","sequence":"first","affiliation":[],"role":[{"vocabulary":"crossref","role":"author"}]},{"ORCID":"https:\/\/orcid.org\/0000-0003-4118-3918","authenticated-orcid":false,"given":"Anton H.J.","family":"de Ruiter","sequence":"additional","affiliation":[],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Krishna Dev","family":"Kumar","sequence":"additional","affiliation":[],"role":[{"vocabulary":"crossref","role":"author"}]}],"member":"263","reference":[{"key":"ref33","doi-asserted-by":"publisher","DOI":"10.1109\/TFUZZ.2005.859306"},{"key":"ref32","doi-asserted-by":"publisher","DOI":"10.1109\/TFUZZ.2008.917301"},{"key":"ref31","doi-asserted-by":"publisher","DOI":"10.1016\/0005-1098(95)00147-6"},{"key":"ref30","doi-asserted-by":"publisher","DOI":"10.1109\/TCST.2013.2246836"},{"key":"ref10","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2015.01.020"},{"key":"ref11","doi-asserted-by":"publisher","DOI":"10.1016\/j.ins.2015.08.042"},{"key":"ref12","doi-asserted-by":"publisher","DOI":"10.1109\/TAES.2015.130725"},{"key":"ref13","doi-asserted-by":"publisher","DOI":"10.1002\/rnc.3554"},{"key":"ref14","doi-asserted-by":"publisher","DOI":"10.1109\/9.286266"},{"key":"ref15","doi-asserted-by":"publisher","DOI":"10.2514\/1.8784"},{"key":"ref16","doi-asserted-by":"publisher","DOI":"10.1109\/ACC.2000.876696"},{"key":"ref17","doi-asserted-by":"publisher","DOI":"10.1016\/j.automatica.2012.05.019"},{"key":"ref18","doi-asserted-by":"publisher","DOI":"10.1016\/j.sysconle.2007.06.011"},{"key":"ref19","doi-asserted-by":"publisher","DOI":"10.1016\/S0005-1098(00)00051-0"},{"key":"ref28","doi-asserted-by":"publisher","DOI":"10.1109\/TAC.2016.2518742"},{"key":"ref4","doi-asserted-by":"publisher","DOI":"10.1109\/TNNLS.2012.2196710"},{"key":"ref27","doi-asserted-by":"publisher","DOI":"10.1109\/9.100933"},{"key":"ref3","doi-asserted-by":"publisher","DOI":"10.2514\/1.46404"},{"key":"ref6","doi-asserted-by":"publisher","DOI":"10.1109\/TIE.2011.2107719"},{"key":"ref29","author":"munkres","year":"1999","journal-title":"Topology"},{"key":"ref5","doi-asserted-by":"publisher","DOI":"10.1109\/TCST.2011.2169796"},{"key":"ref8","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2014.08.009"},{"key":"ref7","doi-asserted-by":"publisher","DOI":"10.1109\/WCICA.2014.7052967"},{"key":"ref2","doi-asserted-by":"publisher","DOI":"10.2514\/1.1059"},{"key":"ref9","doi-asserted-by":"crossref","first-page":"740","DOI":"10.2514\/1.56262","article-title":"Finite-time attitude stabilization for a spacecraft using homogeneous method","volume":"35","author":"li","year":"2012","journal-title":"AIAA J Guid Control Dyn"},{"key":"ref1","doi-asserted-by":"publisher","DOI":"10.2514\/2.4704"},{"key":"ref20","doi-asserted-by":"publisher","DOI":"10.1002\/rnc.3338"},{"key":"ref22","doi-asserted-by":"publisher","DOI":"10.1109\/9.668834"},{"key":"ref21","doi-asserted-by":"publisher","DOI":"10.1109\/TAC.2006.875006"},{"key":"ref24","doi-asserted-by":"publisher","DOI":"10.1016\/0167-6911(92)90078-7"},{"key":"ref23","author":"hardy","year":"1952","journal-title":"Inequalities"},{"key":"ref26","first-page":"439","article-title":"A survey of attitude representations","volume":"41","author":"shuster","year":"1993","journal-title":"J Astron Sci"},{"key":"ref25","author":"hughes","year":"1986","journal-title":"Spacecraft Attitude Dynamics"}],"container-title":["IEEE Transactions on Aerospace and Electronic Systems"],"original-title":[],"link":[{"URL":"http:\/\/xplorestaging.ieee.org\/ielx7\/7\/8637087\/08401917.pdf?arnumber=8401917","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2022,7,13]],"date-time":"2022-07-13T20:46:57Z","timestamp":1657745217000},"score":1,"resource":{"primary":{"URL":"https:\/\/ieeexplore.ieee.org\/document\/8401917\/"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2019,2]]},"references-count":33,"journal-issue":{"issue":"1"},"URL":"https:\/\/doi.org\/10.1109\/taes.2018.2852369","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":[[2019,2]]}}}