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
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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
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HEMLAB Algorithm Applied to HIOCFD Delta Wing and OTC1 Missile
AIAA AVIATION 2023 Forum, 12 Haziran 2023
ASAR İBRAHİM, AKGUN HUSEYİN, ŞAHİN MEHMET
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Predictive missile guidance for agile maneuvering targets with stochastic hybrid dynamics
2016 IEEE Aerospace Conference, 5 Mart 2016
ÜRE NAZIM KEMAL,İNALHAN GÖKHAN
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Three Axes Predictive Control of Autopilot for Missile
Aircraft Engineering and Aerospace Technology, Vol. 88, No. 4
ADA CELAL,KURAL AYHAN
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Predictive Missile Guidance for Agile Maneuvering Targets with Stochastic Hybrid Dynamics
IEEE Aerospace Conference, 5 Mart 2016
ÜRE NAZIM KEMAL,İNALHAN GÖKHAN
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Tactical missile guidance and homing loop applications
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2019
ERDEM TURAN
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Unsteady asymmetric flow separation on missile bodies at high angles of attack
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 1999
TİMUÇİN SERDAROĞLU
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Evasive maneuver trajectory optimization for ucav against air to air missile
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2022
OZAN YAĞCI
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TRACKING OF A BALLISTIC MISSILE DURING REENTRY PHASE WITH UNKNOWN PRIORI-INFORMATION
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2021
MERVE ALSANCAK KABA
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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
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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
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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
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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
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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
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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
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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
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