{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,6,3]],"date-time":"2026-06-03T18:26:20Z","timestamp":1780511180874,"version":"3.54.1"},"reference-count":34,"publisher":"Institute of Electrical and Electronics Engineers (IEEE)","issue":"4","license":[{"start":{"date-parts":[[2018,8,1]],"date-time":"2018-08-01T00:00:00Z","timestamp":1533081600000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/ieeexplore.ieee.org\/Xplorehelp\/downloads\/license-information\/IEEE.html"}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":["IEEE Trans. Aerosp. Electron. Syst."],"published-print":{"date-parts":[[2018,8]]},"DOI":"10.1109\/taes.2018.2798219","type":"journal-article","created":{"date-parts":[[2018,1,25]],"date-time":"2018-01-25T19:20:07Z","timestamp":1516908007000},"page":"1575-1588","source":"Crossref","is-referenced-by-count":47,"title":["Optimal Tracking Guidance for Aeroassisted Spacecraft Reconnaissance Mission Based on Receding Horizon Control"],"prefix":"10.1109","volume":"54","author":[{"given":"Runqi","family":"Chai","sequence":"first","affiliation":[],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Al","family":"Savvaris","sequence":"additional","affiliation":[],"role":[{"vocabulary":"crossref","role":"author"}]},{"ORCID":"https:\/\/orcid.org\/0000-0002-3966-7633","authenticated-orcid":false,"given":"Antonios","family":"Tsourdos","sequence":"additional","affiliation":[],"role":[{"vocabulary":"crossref","role":"author"}]},{"ORCID":"https:\/\/orcid.org\/0000-0003-4083-8863","authenticated-orcid":false,"given":"Senchun","family":"Chai","sequence":"additional","affiliation":[],"role":[{"vocabulary":"crossref","role":"author"}]},{"ORCID":"https:\/\/orcid.org\/0000-0002-5977-4911","authenticated-orcid":false,"given":"Yuanqing","family":"Xia","sequence":"additional","affiliation":[],"role":[{"vocabulary":"crossref","role":"author"}]}],"member":"263","reference":[{"key":"ref33","doi-asserted-by":"publisher","DOI":"10.2514\/1.18196"},{"key":"ref32","doi-asserted-by":"publisher","DOI":"10.2514\/1.33117"},{"key":"ref31","doi-asserted-by":"publisher","DOI":"10.1109\/TAC.2016.2625048"},{"key":"ref30","doi-asserted-by":"publisher","DOI":"10.1109\/TAC.2013.2294618"},{"key":"ref34","doi-asserted-by":"publisher","DOI":"10.1109\/TAC.2015.2505783"},{"key":"ref10","doi-asserted-by":"publisher","DOI":"10.2514\/2.4208"},{"key":"ref11","doi-asserted-by":"publisher","DOI":"10.1002\/oca.711"},{"key":"ref12","doi-asserted-by":"publisher","DOI":"10.2514\/1.A32011"},{"key":"ref13","doi-asserted-by":"publisher","DOI":"10.2514\/3.20009"},{"key":"ref14","doi-asserted-by":"publisher","DOI":"10.1109\/7.220918"},{"key":"ref15","doi-asserted-by":"publisher","DOI":"10.2514\/1.35055"},{"key":"ref16","doi-asserted-by":"publisher","DOI":"10.1109\/TIE.2016.2531021"},{"key":"ref17","doi-asserted-by":"publisher","DOI":"10.1016\/j.actaastro.2016.02.020"},{"key":"ref18","doi-asserted-by":"publisher","DOI":"10.1109\/TAES.2017.2680698"},{"key":"ref19","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2015.06.006"},{"key":"ref28","doi-asserted-by":"publisher","DOI":"10.2514\/1.G001527"},{"key":"ref4","doi-asserted-by":"publisher","DOI":"10.2514\/2.4773"},{"key":"ref27","doi-asserted-by":"publisher","DOI":"10.1109\/TAES.2009.4805267"},{"key":"ref3","doi-asserted-by":"publisher","DOI":"10.2514\/8.9416"},{"key":"ref6","doi-asserted-by":"publisher","DOI":"10.1023\/A:1026454013374"},{"key":"ref29","doi-asserted-by":"publisher","DOI":"10.1109\/TCST.2016.2554524"},{"key":"ref5","doi-asserted-by":"publisher","DOI":"10.2514\/3.21675"},{"key":"ref8","doi-asserted-by":"publisher","DOI":"10.2514\/1.2582"},{"key":"ref7","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2007.01.007"},{"key":"ref2","first-page":"1","article-title":"Optimization of aeroassisted orbital transfer—Current status","volume":"36","author":"mease","year":"1988","journal-title":"J Astronaut Sci"},{"key":"ref9","doi-asserted-by":"publisher","DOI":"10.1016\/S0094-5765(97)00203-8"},{"key":"ref1","doi-asserted-by":"publisher","DOI":"10.2514\/3.25704"},{"key":"ref20","doi-asserted-by":"crossref","first-page":"563","DOI":"10.1016\/j.automatica.2003.11.005","article-title":"A continuation\/GMRES method for fast computation of nonlinear receding\n horizon control","volume":"40","author":"ohtsuka","year":"2004","journal-title":"Automatica"},{"key":"ref22","doi-asserted-by":"publisher","DOI":"10.1016\/j.actaastro.2010.10.010"},{"key":"ref21","doi-asserted-by":"publisher","DOI":"10.1016\/j.isatra.2015.10.015"},{"key":"ref24","doi-asserted-by":"publisher","DOI":"10.1109\/TNNLS.2014.2345734"},{"key":"ref23","doi-asserted-by":"publisher","DOI":"10.1016\/j.asr.2013.01.013"},{"key":"ref26","doi-asserted-by":"publisher","DOI":"10.2514\/1.G002183"},{"key":"ref25","doi-asserted-by":"publisher","DOI":"10.1049\/iet-cta.2014.1198"}],"container-title":["IEEE Transactions on Aerospace and Electronic Systems"],"original-title":[],"link":[{"URL":"http:\/\/xplorestaging.ieee.org\/ielx7\/7\/8428685\/08269278.pdf?arnumber=8269278","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2022,1,26]],"date-time":"2022-01-26T13:04:29Z","timestamp":1643202269000},"score":1,"resource":{"primary":{"URL":"https:\/\/ieeexplore.ieee.org\/document\/8269278\/"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2018,8]]},"references-count":34,"journal-issue":{"issue":"4"},"URL":"https:\/\/doi.org\/10.1109\/taes.2018.2798219","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":[[2018,8]]}}}