Missile Guidance Using Dual-Mode Seeker
學年 100
學期 1
出版(發表)日期 2011-08-01
作品名稱 Missile Guidance Using Dual-Mode Seeker
作品名稱(其他語言)
著者 Ma, Der-Ming; Shiau, Jaw-Kuen; Ho, Ian
單位 淡江大學航空太空工程學系
出版者 Manchester: Scholarlink Resource Centre Ltd.
著錄名稱、卷期、頁數 Journal of Emerging Trends in Engineering and Applied Sciences 2(4), pp.636-642
摘要 This study developed an analytical method to quantitatively analyze the dual-mode seeker guidance performance. The method derives the seekers' measurement models and implements the Kalman filter. The study takes the RF/IR dual-mode seeker, which is proposed for advanced long/medium range air-to-air missiles, as the example. The two-dimensional guidance loop is used to illustrate the methodology and dimensionless equations are derived for generality. After discussing several missile-target scenarios, the results show that the developed scheme provides sufficiently accurate target information for missile guidance, not only for dual-mode seekers, but also when one of the seekers is jammed. The methodology developed in the study can also be applied to increase the accuracy of target tracking.
關鍵字 Dual-mode seeker guidance;IR seeker;Kalman filter;Proportional navigation;RF seeker
語言 en
ISSN 2141-7016
期刊性質 國外
收錄於
產學合作
通訊作者 Ma, Der-Ming
審稿制度
國別 GBR
公開徵稿
出版型式 ,紙本
相關連結

機構典藏連結 ( http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/75810 )

機構典藏連結