Guidance laws against defended aerial targets

Ashwini Ratnoo, Tal Shima

نتاج البحث: فصل من :كتاب / تقرير / مؤتمرمنشور من مؤتمرمراجعة النظراء


The three body engagement scenario is considered where an aerial missile, homing onto a target aircraft, encounters a defender missile launched by the aircraft. A given set of defender missile guidance laws, namely, proportional navigation and line-of-sight guidance are considered and analysis is carried out for proportional navigation and pure pursuit attacking missile strategies. Analytic capture zones and lateral accelerations ratios for the four resulting scenarios are derived. Closed form expression for attacking missile initial position and launch angles are derived for a successful evasion from the defender. Extensive numerical simulations are carried out which comply with the analytical findings.

اللغة الأصليةالإنجليزيّة
عنوان منشور المضيفAIAA Guidance, Navigation, and Control Conference 2011
المعرِّفات الرقمية للأشياء
حالة النشرنُشِر - 2011
الحدثAIAA Guidance, Navigation and Control Conference 2011 - Portland, OR, الولايات المتّحدة
المدة: ٨ أغسطس ٢٠١١١١ أغسطس ٢٠١١

سلسلة المنشورات

الاسمAIAA Guidance, Navigation, and Control Conference 2011


!!ConferenceAIAA Guidance, Navigation and Control Conference 2011
الدولة/الإقليمالولايات المتّحدة
المدينةPortland, OR

All Science Journal Classification (ASJC) codes

  • !!Aerospace Engineering
  • !!Control and Systems Engineering
  • !!Electrical and Electronic Engineering


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