DC Field | Value | Language |
---|---|---|
dc.contributor.author | Ryu, S.-M. | - |
dc.contributor.author | Won, D.-Y. | - |
dc.contributor.author | Lee, C.-H. | - |
dc.contributor.author | Tahk, Min-Jea | - |
dc.date.accessioned | 2013-03-28T09:52:39Z | - |
dc.date.available | 2013-03-28T09:52:39Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 2010-06-08 | - |
dc.identifier.citation | 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010, v., no., pp.535 - 539 | - |
dc.identifier.uri | http://hdl.handle.net/10203/164682 | - |
dc.language | ENG | - |
dc.title | High angle of attack missile autopilot design by pole placement approach | - |
dc.type | Conference | - |
dc.identifier.scopusid | 2-s2.0-79952136837 | - |
dc.type.rims | CONF | - |
dc.citation.beginningpage | 535 | - |
dc.citation.endingpage | 539 | - |
dc.citation.publicationname | 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010 | - |
dc.identifier.conferencecountry | China | - |
dc.identifier.conferencecountry | China | - |
dc.contributor.localauthor | Tahk, Min-Jea | - |
dc.contributor.nonIdAuthor | Ryu, S.-M. | - |
dc.contributor.nonIdAuthor | Won, D.-Y. | - |
dc.contributor.nonIdAuthor | Lee, C.-H. | - |
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