Tezin Türü: Yüksek Lisans
Tezin Yürütüldüğü Kurum: Orta Doğu Teknik Üniversitesi, Fen Bilimleri Enstitüsü, Türkiye
Tezin Onay Tarihi: 2014
Tezin Dili: İngilizce
Öğrenci: TAYFUN ÇELİK
Asıl Danışman (Eş Danışmanlı Tezler İçin): Ender Ciğeroğlu
Eş Danışman: Yiğit Yazıcıoğlu
Özet:Air-to-air missiles require high maneuverability. In order to obtain high maneuverability, hybrid fin actuation systems are used. In this study, a hybrid fin actuation system which is composed of aerodynamic control surfaces and thrust vector control is designed. Both aerodynamic and thrust vector control types are explained and the most suitable pair is determined for air-to-air missile. Then, the designed system is physically constructed and system identification procedure is performed. After that three different controllers PID, H∞ and 2-DOF H∞ controllers are designed and tested on both on the real system and simulation environment. Finally, all the results are compared with the cascaded H∞ controller.