Launch Time Window Determination for Missile Interceptor

碩士 === 國立交通大學 === 電控工程研究所 === 99 === When an attacking missile is detected, the missile defense system must decide when to launch the missile interceptor. The choice of a proper launch time is important because given the physical constraints on the interceptor, a poor choice of launch time alone may...

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Main Authors: Lin, Yen-Po, 林彥伯
Other Authors: Lin, Ching-An
Format: Others
Language:zh-TW
Published: 2010
Online Access:http://ndltd.ncl.edu.tw/handle/62899332894810223587
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spelling ndltd-TW-099NCTU54490102016-04-18T04:21:46Z http://ndltd.ncl.edu.tw/handle/62899332894810223587 Launch Time Window Determination for Missile Interceptor 攔截飛彈的發射時間窗口決定 Lin, Yen-Po 林彥伯 碩士 國立交通大學 電控工程研究所 99 When an attacking missile is detected, the missile defense system must decide when to launch the missile interceptor. The choice of a proper launch time is important because given the physical constraints on the interceptor, a poor choice of launch time alone may cause the interception to fail. This thesis discusses the determination of launch time window for a missile interceptor, which is formulated as constrained optimization problems. The earliest and the latest allowable launch times are determined by numerically solve the corresponding minimization and maximization problems. Three incoming threats are considered. Numerical results show good agreement with results obtained via six degree of freedom simulations employing midcourse guidance. Lin, Ching-An 林清安 2010 學位論文 ; thesis 94 zh-TW
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language zh-TW
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description 碩士 === 國立交通大學 === 電控工程研究所 === 99 === When an attacking missile is detected, the missile defense system must decide when to launch the missile interceptor. The choice of a proper launch time is important because given the physical constraints on the interceptor, a poor choice of launch time alone may cause the interception to fail. This thesis discusses the determination of launch time window for a missile interceptor, which is formulated as constrained optimization problems. The earliest and the latest allowable launch times are determined by numerically solve the corresponding minimization and maximization problems. Three incoming threats are considered. Numerical results show good agreement with results obtained via six degree of freedom simulations employing midcourse guidance.
author2 Lin, Ching-An
author_facet Lin, Ching-An
Lin, Yen-Po
林彥伯
author Lin, Yen-Po
林彥伯
spellingShingle Lin, Yen-Po
林彥伯
Launch Time Window Determination for Missile Interceptor
author_sort Lin, Yen-Po
title Launch Time Window Determination for Missile Interceptor
title_short Launch Time Window Determination for Missile Interceptor
title_full Launch Time Window Determination for Missile Interceptor
title_fullStr Launch Time Window Determination for Missile Interceptor
title_full_unstemmed Launch Time Window Determination for Missile Interceptor
title_sort launch time window determination for missile interceptor
publishDate 2010
url http://ndltd.ncl.edu.tw/handle/62899332894810223587
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