{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,10,31]],"date-time":"2026-10-31T22:02:49Z","timestamp":1793484169565,"version":"4.5.0"},"reference-count":34,"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"}],"funder":[{"name":"Science Center Program of National Natural Science Foundation of China","award":["62188101"],"award-info":[{"award-number":["62188101"]}]}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":["IEEE Trans. Aerosp. Electron. Syst."],"published-print":{"date-parts":[[2024,6]]},"DOI":"10.1109\/taes.2024.3360948","type":"journal-article","created":{"date-parts":[[2024,2,1]],"date-time":"2024-02-01T19:00:34Z","timestamp":1706814034000},"page":"3379-3389","source":"Crossref","is-referenced-by-count":26,"title":["Discrete-Time High-Order Fully Actuated Adaptive Stabilization Control for a Type of Combined Spacecraft With Unknown Parameters"],"prefix":"10.1109","volume":"60","author":[{"ORCID":"https:\/\/orcid.org\/0000-0003-2262-7050","authenticated-orcid":false,"given":"Kai-Xin","family":"Cui","sequence":"first","affiliation":[{"name":"Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"ORCID":"https:\/\/orcid.org\/0000-0002-8169-2218","authenticated-orcid":false,"given":"Guang-Ren","family":"Duan","sequence":"additional","affiliation":[{"name":"Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"ORCID":"https:\/\/orcid.org\/0000-0003-4993-048X","authenticated-orcid":false,"given":"Da-Wei","family":"Zhang","sequence":"additional","affiliation":[{"name":"Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"ORCID":"https:\/\/orcid.org\/0000-0003-0611-5004","authenticated-orcid":false,"given":"Da-Ke","family":"Gu","sequence":"additional","affiliation":[{"name":"School of Automation Engineering, Northeast Electric Power University, Jilin, China"}],"role":[{"vocabulary":"crossref","role":"author"}]}],"member":"263","reference":[{"key":"ref1","doi-asserted-by":"publisher","DOI":"10.1016\/j.actaastro.2020.10.033"},{"key":"ref2","doi-asserted-by":"publisher","DOI":"10.1080\/00207179.2018.1479775"},{"key":"ref3","doi-asserted-by":"publisher","DOI":"10.1155\/2020\/3648260"},{"key":"ref4","doi-asserted-by":"publisher","DOI":"10.1016\/j.isatra.2018.01.016"},{"issue":"2","key":"ref5","first-page":"1","article-title":"On-orbit intelligent identification of combined spacecraft s inertia parameter based on deep learning","volume":"39","author":"Jin","year":"2019","journal-title":"Chin. Space Sci. Technol."},{"key":"ref6","doi-asserted-by":"publisher","DOI":"10.1016\/j.neucom.2021.07.099"},{"key":"ref7","doi-asserted-by":"publisher","DOI":"10.1002\/rnc.4693"},{"key":"ref8","doi-asserted-by":"crossref","DOI":"10.1007\/978-1-84800-066-7","volume-title":"Nonlinear and Adaptive Control With Applications","author":"Astolfi","year":"2008"},{"key":"ref9","doi-asserted-by":"publisher","DOI":"10.1016\/j.isatra.2021.02.017"},{"key":"ref10","doi-asserted-by":"publisher","DOI":"10.1016\/j.automatica.2023.111250"},{"key":"ref11","doi-asserted-by":"publisher","DOI":"10.1002\/rnc.679"},{"key":"ref12","doi-asserted-by":"publisher","DOI":"10.1016\/j.actaastro.2020.05.013"},{"key":"ref13","doi-asserted-by":"publisher","DOI":"10.1109\/JSEE.2014.00075"},{"key":"ref14","doi-asserted-by":"publisher","DOI":"10.1007\/s12555-016-0696-0"},{"key":"ref15","doi-asserted-by":"publisher","DOI":"10.1080\/00207179.2017.1340672"},{"key":"ref16","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2014.11.013"},{"key":"ref17","doi-asserted-by":"publisher","DOI":"10.1109\/TAES.2022.3164011"},{"key":"ref18","doi-asserted-by":"publisher","DOI":"10.1061\/(ASCE)AS.1943-5525.0001040"},{"key":"ref19","doi-asserted-by":"publisher","DOI":"10.1080\/00207721.2020.1829167"},{"issue":"7","key":"ref20","first-page":"1333","article-title":"High-order system approaches: I. Fully-actuated systems and parametric designs (in Chinese)","volume":"46","author":"Duan","year":"2020","journal-title":"Acta Automatica Sinica"},{"key":"ref21","doi-asserted-by":"publisher","DOI":"10.1080\/00207721.2020.1849863"},{"key":"ref22","doi-asserted-by":"publisher","DOI":"10.1007\/s11424-022-2045-0"},{"key":"ref23","doi-asserted-by":"publisher","DOI":"10.1080\/00207721.2020.1849864"},{"key":"ref24","doi-asserted-by":"publisher","DOI":"10.1007\/s11424-022-2019-2"},{"key":"ref25","doi-asserted-by":"publisher","DOI":"10.1109\/TCSII.2022.3177309"},{"key":"ref26","doi-asserted-by":"publisher","DOI":"10.1016\/j.automatica.2023.110969"},{"key":"ref27","doi-asserted-by":"publisher","DOI":"10.1016\/j.jfranklin.2023.05.010"},{"key":"ref28","doi-asserted-by":"publisher","DOI":"10.1080\/00207721.2021.1975848"},{"key":"ref29","doi-asserted-by":"publisher","DOI":"10.1007\/s11424-022-2046-z"},{"key":"ref30","doi-asserted-by":"publisher","DOI":"10.1109\/TMECH.2022.3223927"},{"key":"ref31","doi-asserted-by":"publisher","DOI":"10.1109\/TSMC.2022.3188504"},{"issue":"1","key":"ref32","first-page":"628892","article-title":"High-order fully actuated anti-disturbance control for a type of combined spacecraft based on disturbance observer (in Chinese)","volume":"45","author":"Cui","year":"2024","journal-title":"Acta Aeronautica et Astronautica Sinica"},{"key":"ref33","doi-asserted-by":"publisher","DOI":"10.1109\/CDC.2005.1583211"},{"issue":"7","key":"ref34","first-page":"839","article-title":"Quasi-linear system approaches for flight vehicle control  Part 2: Methods and prospects (in Chinese)","volume":"41","author":"Duan","year":"2020","journal-title":"J. Astronaut."}],"container-title":["IEEE Transactions on Aerospace and Electronic Systems"],"original-title":[],"link":[{"URL":"http:\/\/xplorestaging.ieee.org\/ielx7\/7\/10552647\/10418530.pdf?arnumber=10418530","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2024,6,25]],"date-time":"2024-06-25T21:04:13Z","timestamp":1719349453000},"score":1,"resource":{"primary":{"URL":"https:\/\/ieeexplore.ieee.org\/document\/10418530\/"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2024,6]]},"references-count":34,"journal-issue":{"issue":"3"},"URL":"https:\/\/doi.org\/10.1109\/taes.2024.3360948","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]]}}}