Differential game theory application to intelligent missile guidance
Date
2013
Authors
Faruqi, F.
Rajagopalan, A.
Nandagopal, D.N.
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Conference paper
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2013 2nd IEEE Conference on Control, Systems & Industrial Informatics (ICCSII), 2013, pp.7-13
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2nd IEEE Conference on Control, Systems & Industrial Informatics (23 Jun 2013 - 26 Jun 2013 : Bandung, Indonesia)
Abstract
This paper considers a missile guidance problem where an aircraft target that is being engaged by a ground launched missile, fires a defending missile against this attacker and itself performs a manoeuvre to escape the attacking missile. In order to engage the aircraft, the attacking missile performs, both, an evasive manoeuvre to defeat (evade) the defending missile and an intercept manoeuvre to engage the aircraft target. Differential game theoretic approach is proposed that utilizes a linear quadratic performance index optimization technique to obtain guidance strategies for the parties; guidance strategies obtained are used in a 3-D simulation, to study the characteristics of the resulting intercept and evasion strategies. Simple (rule based) AI technique is proposed for implementing additional manoeuvres to enable the parties to enhance their evasion/survival or, in the case of the attacker to achieve intercept.
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Copyright 2013 IEEE