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dc.contributor.authorZhang, Yen_US
dc.contributor.authorVepa, Ren_US
dc.contributor.authorLi, Gen_US
dc.contributor.authorZeng, Ten_US
dc.date.accessioned2018-11-23T11:53:14Z
dc.date.available2018-07-25en_US
dc.date.issued2019-08en_US
dc.date.submitted2018-08-03T15:24:50.790Z
dc.identifier.issn0018-9251en_US
dc.identifier.urihttp://qmro.qmul.ac.uk/xmlui/handle/123456789/53084
dc.format.extent2001 - 2011en_US
dc.relation.ispartofIEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMSen_US
dc.titleMars Powered Descent Phase Guidance Design Based on Fixed-Time Stabilization Techniqueen_US
dc.typeArticle
dc.rights.holder© 2018 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.
dc.identifier.doi10.1109/TAES.2018.2880051en_US
pubs.author-urlhttp://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcApp=PARTNER_APP&SrcAuth=LinksAMR&KeyUT=WOS:000480348800032&DestLinkType=FullRecord&DestApp=ALL_WOS&UsrCustomerID=612ae0d773dcbdba3046f6df545e9f6aen_US
pubs.issue4en_US
pubs.notesNot knownen_US
pubs.publication-statusPublisheden_US
pubs.volume55en_US


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