Application of modern guidance control theory to a back-to-turn missile.

Bibliographic Details
Main Author:	Shin, Bohyun
Other Authors:	NA
Language:	en_US
Published:	Monterey, California. Naval Postgraduate School 2012
Online Access:	http://hdl.handle.net/10945/19161

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spelling	ndltd-nps.edu-oai-calhoun.nps.edu-10945-191612014-11-27T16:13:08Z Application of modern guidance control theory to a back-to-turn missile. Shin, Bohyun NA NA NA 2012-11-19T23:48:43Z 2012-11-19T23:48:43Z 1984 Thesis http://hdl.handle.net/10945/19161 ocn640242307 en_US Monterey, California. Naval Postgraduate School
collection	NDLTD
language	en_US
sources	NDLTD
author2	NA
author_facet	NA Shin, Bohyun
author	Shin, Bohyun
spellingShingle	Shin, Bohyun Application of modern guidance control theory to a back-to-turn missile.
author_sort	Shin, Bohyun
title	Application of modern guidance control theory to a back-to-turn missile.
title_short	Application of modern guidance control theory to a back-to-turn missile.
title_full	Application of modern guidance control theory to a back-to-turn missile.
title_fullStr	Application of modern guidance control theory to a back-to-turn missile.
title_full_unstemmed	Application of modern guidance control theory to a back-to-turn missile.
title_sort	application of modern guidance control theory to a back-to-turn missile.
publisher	Monterey, California. Naval Postgraduate School
publishDate	2012
url	http://hdl.handle.net/10945/19161
work_keys_str_mv	AT shinbohyun applicationofmodernguidancecontroltheorytoabacktoturnmissile
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