Missile Guidance Using Dual-Mode Seeker

機構典藏 > College of Engineering > Graduate Institute & Department of Aerospace Engineering > Journal Article > Item 987654321/75810

Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/75810

Title:	Missile Guidance Using Dual-Mode Seeker
Authors:	Ma, Der-Ming;Shiau, Jaw-Kuen;Ho, Ian
Contributors:	淡江大學航空太空工程學系
Keywords:	Dual-mode seeker guidance;IR seeker;Kalman filter;Proportional navigation;RF seeker
Date:	2011-08
Issue Date:	2013-03-20 16:36:41 (UTC+8)
Publisher:	Manchester: Scholarlink Resource Centre Ltd.
Abstract:	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.
Relation:	Journal of Emerging Trends in Engineering and Applied Sciences 2(4), pp.636-642
Appears in Collections:	[Graduate Institute & Department of Aerospace Engineering] Journal Article

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