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Helikopterler için Sinir Ağı Tabanlı Adaptif Kontrolcü Tasarımında Ağırlık erkezi Modelleme Hatasının Önemi
Date
2008-11-13
Author
Yavrucuk, İlkay
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https://hdl.handle.net/11511/88069
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Development of a comprehensive and modular modelling, analysis and simulation tool for helicopters
Yücekayalı, Arda; Kutay, Ali Türker; Department of Aerospace Engineering (2011)
Helicopter flight dynamic, rotor aerodynamic and dynamic analyses activities have been a great dispute since the first helicopters, at both design and test stages. Predicting rotor aerodynamic and dynamic characteristics, helicopter dynamic behavior and trimmed flight conditions is a huge challenge to engineers as it involves the tradeoff between accuracy, fidelity, complexity and computational cost. Flight dynamic activities such as; predicting trim conditions, helicopter dynamic behavior and simulation of...
Helikopter Simülatörleri için Dinamik Turboşaft Motor Modeli Geliştirilmesi ve Simülatöre Entegrasyonu
Uzol, Oğuz; Yavrucuk, İlkay (2013-06-11)
Helikopter Pal Ucu Şekillerinin Aerodinamik Performansa ve Uç Girdabına Etkisinin Deneysel Olarak İncelenmesi
Uluocak, Sinem; Hazaveh, Hooman Amiri; Perçin, Mustafa; Akpolat, M Tuğrul; Uzol, Oğuz (null; 2018-09-14)
Helikopter Otopilotları için Yaklışma Üst Modu Tasarımı ve Simülasyonu
Yavrucuk, İlkay (null; 2013-06-11)
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İ. Yavrucuk, “Helikopterler için Sinir Ağı Tabanlı Adaptif Kontrolcü Tasarımında Ağırlık erkezi Modelleme Hatasının Önemi,” 2008, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/88069.