Taktik Füzelerde Kullanılan Sonlanma Güdümü Yöntemlerinin 3B Formülasyonları ve Analizi

Abstract

This thesis aims to develop dynamical formulations of terminal guidance of tactical missiles in 3-dimensional engagement setting. The guidance methods studied in this thesis are; proportional navigation, pursuit guidance, CLOS and beam riding guidance. Some modifications faciliating improved performance in realistic situations are proposed for CLOS and beam riding guidance. Performance of the proposed guidance methods are studied via computer simulations as well as by using adjoint analysis.