Çoklu Füze Sistemleri için Güdüm Algoritması Tasarımı

Year 2021, Volume: 23 Issue: 68, 469 - 477, 24.05.2021

Raziye Tekin Koray Savaş Erer

https://doi.org/10.21205/deufmd.2021236810

Abstract

Bu çalışmada, çoklu otonom sistemler için güdüm algoritma tasarımları sunulmuştur. Otonom sistem olarak jenerik bir füze ele alınmıştır. İlk olarak, eş zamanlı varış kontrolü için menzilin zamana bağlı genel bir polinom olarak şekillendirildiği bir güdüm tasarımı sunulmuştur. Sonrasında bir lider ve takipçilerden oluşan bir sistem için füze güdümü kullanılarak bir takip algoritması tasarımı önerilmiştir. Bunun için varış açısının kontrolünü sağlayan bir yöntem, lidere göre sabit olarak konumlandırılan bir sanal lideri kuyruk takibi modunda izlemek için kullanılmıştır. Her iki ortak saldırı yaklaşımında, otonom sisteme yeni üyeler, görev tanımları merkezi kontrol birimi ya da lider tarafından tanımlanarak dahil olabilirler. Önerilen yaklaşımlar füzeler için örneklenmiş olup, insansız hava araçlarında ve robotik alanında da kullanılabilir.

Keywords

Çoklu otonom sistemler, Füze güdümü, Ortak saldırı, Varış zamanı, Varış açısı, Kuyruk takibi

Guidance Algorithm Design for Multi-Missile Systems

Abstract

In this paper, guidance algorithms design for multi-autonomous systems is described. A generic missile is considered as an autonomous system. First, a guidance law, where the range is shaped as a function of time, is presented for salvo attack. Second, a tracking algorithm, which makes use of missile guidance algorithms, is proposed for a system consisting of a leader and followers. For this purpose, an impact angle control algorithm is used for tail chase tracking of the leader, where a virtual leader is attached to a fixed position of the leader. In each of these two approaches, new members can join the system, where the mission is defined from a central control unit or from a leader. The suggested approached is exemplified for missiles; however, they could be used in unmanned air vehicles and in robotics.

Keywords

Multi-autonomous systems, Missile guidance, Salvo attack, Impact time, Impact angle, Tail tracking

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