ARAMA SONUÇLARI

Toplam 13 adet sonuçtan 13 tanesi görüntülenmektedir.

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

Melike Nikbay Tam metin bildiri UCAVmissiletrajectoryevasive

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

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

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

Missile evasion maneuver generation with model-free deep reinforcement learning

Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2024

MUHAMMED MURAT ÖZBEK

Emre Koyuncu 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

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

Seher Eken Özgün Makale CONCENTRATED MASSROTATING SHAFTROCKET THRUSTSTABILITYVIBRATIONMISSILE

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

ADAPTIVE CONTROL OF MISSILE-TARGET ENGAGEMENT PROBLEM VIA PROPORTIONAL NAVIGATION GUIDANCE

2th International Black Sea Modern Scientific Research Congress, Rize/TÜRKİYE, 21 Aralık 2022, s. 67-81

KARA AHMET, UÇAK KEMAL

Kemal Uçak Tam metin bildiri

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