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...
Main Authors: | , |
---|---|
Other Authors: | |
Format: | Others |
Language: | zh-TW |
Published: |
2010
|
Online Access: | http://ndltd.ncl.edu.tw/handle/62899332894810223587 |
id |
ndltd-TW-099NCTU5449010 |
---|---|
record_format |
oai_dc |
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 |
collection |
NDLTD |
language |
zh-TW |
format |
Others
|
sources |
NDLTD |
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 |
work_keys_str_mv |
AT linyenpo launchtimewindowdeterminationformissileinterceptor AT línyànbó launchtimewindowdeterminationformissileinterceptor AT linyenpo lánjiéfēidàndefāshèshíjiānchuāngkǒujuédìng AT línyànbó lánjiéfēidàndefāshèshíjiānchuāngkǒujuédìng |
_version_ |
1718227113628139520 |