Powered Descent Guidance for Mars Pinpoint Landing Based on Model Predictive Control Theory

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dc.contributor.authorJung, Youeyunko
dc.contributor.authorBang, Hyo Choongko
dc.date.accessioned2016-07-07T08:09:09Z-
dc.date.available2016-07-07T08:09:09Z-
dc.date.created2016-01-04-
dc.date.issued2015-11-26-
dc.identifier.citation2015 Asia-Pacific international Symposium on Aerospace Technology(APISAT)-
dc.identifier.urihttp://hdl.handle.net/10203/210322-
dc.languageEnglish-
dc.publisher2015 Asia-Pacific international Symposium on Aerospace Technology(APISAT)-
dc.titlePowered Descent Guidance for Mars Pinpoint Landing Based on Model Predictive Control Theory-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.publicationname2015 Asia-Pacific international Symposium on Aerospace Technology(APISAT)-
dc.identifier.conferencecountryAT-
dc.identifier.conferencelocationHilton Cairns, Queensland-
dc.contributor.localauthorBang, Hyo Choong-
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AE-Conference Papers(학술회의논문)
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