The effect of acceleration and deceleration on the dynamic stability of a missile

Bibliographic Details
Main Author:	Steinmetz, William John
Format:	Others
Language:	en_US
Published:	Georgia Institute of Technology 2006
Subjects:	Guided missiles Stability Oscillations
Online Access:	http://hdl.handle.net/1853/12262

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spelling	ndltd-GATECH-oai-smartech.gatech.edu-1853-122622013-12-15T03:33:02ZThe effect of acceleration and deceleration on the dynamic stability of a missileSteinmetz, William JohnGuided missilesStabilityOscillationsGeorgia Institute of Technology2006-10-20T15:16:02Z2006-10-20T15:16:02Z1962-12Thesis243 bytestext/htmlhttp://hdl.handle.net/1853/12262784742en_USAccess restricted to authorized Georgia Tech users only.
collection	NDLTD
language	en_US
format	Others
sources	NDLTD
topic	Guided missiles Stability Oscillations
spellingShingle	Guided missiles Stability Oscillations Steinmetz, William John The effect of acceleration and deceleration on the dynamic stability of a missile
author	Steinmetz, William John
author_facet	Steinmetz, William John
author_sort	Steinmetz, William John
title	The effect of acceleration and deceleration on the dynamic stability of a missile
title_short	The effect of acceleration and deceleration on the dynamic stability of a missile
title_full	The effect of acceleration and deceleration on the dynamic stability of a missile
title_fullStr	The effect of acceleration and deceleration on the dynamic stability of a missile
title_full_unstemmed	The effect of acceleration and deceleration on the dynamic stability of a missile
title_sort	effect of acceleration and deceleration on the dynamic stability of a missile
publisher	Georgia Institute of Technology
publishDate	2006
url	http://hdl.handle.net/1853/12262
work_keys_str_mv	AT steinmetzwilliamjohn theeffectofaccelerationanddecelerationonthedynamicstabilityofamissile AT steinmetzwilliamjohn effectofaccelerationanddecelerationonthedynamicstabilityofamissile
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The effect of acceleration and deceleration on the dynamic stability of a missile

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