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Özel Aralık Girişi

Evasive Maneuver Trajectory Optimization of an UCAV Against an Air to Air Missile
2022 AIAA Aviation Forum, Chicago/AMERİKA BİRLEŞİK DEVLETLERİ, 27 Haziran 2022
YAĞCI OZAN, NİKBAY MELİKE
Adaptive fuzzy based threat evaluation method for air and missile defense systems
Elsevier BV, Vol. 643, Eylül 2023, ISSN: 0020-0255
TUNCER ÖZGÜR, ÇIRPAN HAKAN ALİ
Hakan Ali Çırpan Özgün Makale
HEMLAB Algorithm Applied to HIOCFD Delta Wing and OTC1 Missile
AIAA AVIATION 2023 Forum, 12 Haziran 2023
ASAR İBRAHİM, AKGUN HUSEYİN, ŞAHİN MEHMET
Mehmet Şahin Tam metin bildiri
Predictive missile guidance for agile maneuvering targets with stochastic hybrid dynamics
2016 IEEE Aerospace Conference, 5 Mart 2016
ÜRE NAZIM KEMAL,İNALHAN GÖKHAN
Nazım Kemal Üre Tam metin bildiri
Three Axes Predictive Control of Autopilot for Missile
Aircraft Engineering and Aerospace Technology, Vol. 88, No. 4
ADA CELAL,KURAL AYHAN
Ayhan Kural Özgün Makale
Predictive Missile Guidance for Agile Maneuvering Targets with Stochastic Hybrid Dynamics
IEEE Aerospace Conference, 5 Mart 2016
ÜRE NAZIM KEMAL,İNALHAN GÖKHAN
Gökhan İnalhan Tam metin bildiri
Tactical missile guidance and homing loop applications
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2019
ERDEM TURAN
Cengiz Hacızade Tez Yüksek Lisans Tamamlandı
Unsteady asymmetric flow separation on missile bodies at high angles of attack
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 1999
TİMUÇİN SERDAROĞLU
İlyas Bedii Özdemir Tez Yüksek Lisans Tamamlandı
Evasive maneuver trajectory optimization for ucav against air to air missile
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2022
OZAN YAĞCI
Melike Nikbay Tez Yüksek Lisans Tamamlandı
TRACKING OF A BALLISTIC MISSILE DURING REENTRY PHASE WITH UNKNOWN PRIORI-INFORMATION
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2021
MERVE ALSANCAK KABA
İlker Murat Koç Tez Yüksek Lisans Devam Ediyor
Output redefinition method for sliding mode control of nonminimum phase missile systems
2015 7th International Conference on Recent Advances in Space Technologies (RAST), Istanbul, Turkey/TÜRKİYE, 16 Haziran 2015
PARALI YAĞIZ,JAFAROV ELBRUS
Elbrus Jafarov Tam metin bildiri
Higher order sliding mode control applications with output redefinition for nonminimum phase missile system
2015 International Workshop on Recent Advances in Sliding Modes (RASM), Istanbul, Turkey/TÜRKİYE, 9 Nisan 2015
PARALI YAĞIZ,JAFAROV ELBRUS
Elbrus Jafarov Tam metin bildiri
Predictive Missile Guidance with Online Trajectory Learning
Defence Science Journal, Vol. 67, No. 3, Nisan 2017, s. 332, ISSN: 0976464X
AKÇAL MEHMET UĞUR,ÜRE NAZIM KEMAL
Nazım Kemal Üre Özgün Makale
Dynamic instability of spinning launch vehicles modeled as thin-walled composite beams
ACTA MECHANICA, Vol. 228, No. 12, Aralık 2017, s. 4353-4367, ISSN: 0001-5970
CİHAN MELAHAT, EKEN SEHER, KAYA METİN ORHAN
Missile Evasion Maneuver Generation with Model-free Deep Reinforcement Learning
10th International Conference on Recent Advances in Air and Space Technologies (RAST), 7 Haziran 2023
ÖZBEK MURAT, KOYUNCU EMRE
Emre Koyuncu Tam metin bildiri
Design and comparison of autopilots of an air to surface antitank missile and its terminal guidance study
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 228, No. 2, Şubat 2014, s. 193-205
ADA CELAL, KURAL AYHAN
Ayhan Kural Özgün Makale
Design of Robust Autopilot Output Integral Sliding Mode Controllers for Guided Missile Systems
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, Vol. 73, No. 1, Ocak 2001, s. 16-25, ISSN: 1748-8842
JAFAROV ELBRUS,TAŞALTIN RAMAZAN
Elbrus Jafarov Özgün Makale

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