Güncel Gönderiler: Sivil Havacılık Yüksekokulu
Toplam kayıt 105, listelenen: 1-20
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Türkiye'de bölgesel havayolu taşımacılığının geliştirilmesi için yapılması gerekenler
(2011)Bölgesel havayolu taşımacılığı dünyada çok önemli bir role sahip olan havayolu taşımacılığının en hızlı büyüyen bölümlerinden birisidir. Nispeten küçük kapasiteli uçaklarla genellikle büyük ve küçük yerleşim yerleri arasında, ... -
Türkiye'de havaaracı bakım faaliyetlerinde dış kaynak kullanımı üzerine bir araştırma
(2012)Günümüzde işletmeler giderek artan bir biçim-de, sadece sahip oldukları yetenek ve becerileri esas alan işlere odaklanmakta, diğer faaliyetleri ise dış kaynaklardan sağlamaktadırlar. İşletmeler dış kaynak kullanımı sayesinde ... -
Avrupa Birliği'ne tam üyelik sürecinde Türkiye-Avrupa Birliği havayolu pazarındaki ekonomik düzenlemelerin havayolu yönetimine etkisi açısından incelenmesi
(2012)Rekabetin çok yoğun yaşandığı liberal pazarlar havayolu işletmelerinin genel ve rekabet stratejilerini doğrudan etkilemektedir. Türkiye Avrupa Birliği'ne tam üye olduğunda Türk Tescilli Havayolu İşletmeleri dünyanın en ... -
Uçakların Yanlamasına Hareketlerinin Gözleyiciler ve Kalman Filtresi ile Durum Kestirimi
(2009)Günümüzde, pek çok iş modelleme yapılması sayesinde kolaylaşmaktadır. Gerçek sistemlerle çalışmak yerine, modelleme kullanılarak, gerçek sistem davranışları incelenebilir ve analiz edilebilir. Arıza toleranslı bir yapı ... -
An integrated navigation system design for Quadrotors
(Institute of Electrical and Electronics Engineers Inc., 2015)In this work, a particle filter based integrated navigation system is designed and tested with real quadrotor systems. Conventionally, Kalman filter based algorithms is used for navigation systems which is highly non-linear. ... -
Historical development of UAV technologies in the world: The case of Turkey
(Springer International Publishing, 2016)The new technologies and designs on Unmanned Aerial Vehicles (UAVs) have created a new market which made it possible for many countries to compete by penetrating and dominating the market. The new advances in computer and ... -
The modeling and simulation of a quadrocopter
(EUROSIS, 2016)Mini-flying vehicles with four rotors which are called quadcopters have attracted many researchers in recent years. Quadrotor is the one of the most popular rotary wing aircraft in control problems. Vertical take off and ... -
Modelling and pid controller design for a quadrotor
(EUROSIS, 2016)This paper presents the modelling of a four rotor vertical take-off and landing unmanned air vehicle known as the quadrotor aircraft, Vertical take off and landing, high maneuverability capabilities and indoor/outdoor ... -
Zaman Serilerinde NARX Sinir Ağları Modeliyle Uçuşa Elverişlilik Süresinin Kestirimi
(Institute of Electrical and Electronics Engineers Inc., 2017)Havacılık planlamalara yo˘gun bir ¸sekilde ba¸svurulan ciddi bir sektördür. Yüksek maliyetlere sebep olabilecek plansızlı˘gın giderilmesi ve vahim sonuçlar do˘gurabilecek kazaların önüne geçilebilmesi için öngörülere ... -
Comparison of classical PD and fuzzy PD controller performances of an aircraft pitch angle control system
(2011)Aircraft dynamics are in general nonlinear, time varying, and uncertain. A control system (classical control systems) designed for a flight condition, may not provide the desired stability and performance characteristics ... -
PID controlling of the Quadrotor and sensor performance tests
(World Scientific and Engineering Academy and Society, 2014)This paper includes three main parts. The first part is about a Quadrotor as a type of unmanned vehicles. The second part includes its mathematical model and controlling with PID controller. The last part consists of some ... -
The importance of preventive maintenance in terms of reliability in aviation sector
(2011)Aircraft is a system that requires high reliability levels throughout flights. Preventive maintenance procedures are applied to maintain this reliability at an optimum level. The higher frequency of preventive maintenance ... -
Performance comparison of yaw rate damping controllers
(2013)Maintaining desired flight conditions in flight envelope for a long period is one of the primary control problems in aircraft flight control. Aircraft dynamics are in general nonlinear, time varying and uncertain. A control ... -
Aircraft engine sensor fault detection, isolaton and reconfiguration using fuzzy logic control based unknown input observer
(Lappeenranta University of Technology, 2014)In this paper, a model-based robust fault diagnosis approach 'Unknown Input Observer (UIO)', 'Generalized Observer Scheme (GOS)' and 'a Fuzzy Logic Control Mechanism' will be studied respectively for fault detection, ... -
Design of fault tolerant flight control system
(2010)The purpose of the paper is to present an approach to detect, isolate and accommodate the sensor or actuator faults using bank of observer and unknown input observers (UIO). Full order observers, reduced order observers, ... -
A fault tolerant flight control system for sensor and actuator faults
(2010)The purpose of the paper is to present an approach to detect, isolate and accommodate the sensor or actuator faults using bank of unknown input observers (UIO). Full order observers, reduced order observers, unknown input ... -
ARINC 629 data bus standard on aircrafts
(2010)In earlier analogue avionic systems the number of cables used to transfer information between the various system components was considerable. With these systems, at least one pair of wires has been required for each signal ... -
NARX Neural Networks Based Time Series Prediction for Amount of Airworthiness Time
(IEEE, 2016)Aviation, a serious sector, is required to recourse planning intensively. There is a need for foresight in order to eliminate the planless that can lead to high costs and prevent accidents that could cause to fatal ... -
Pitch rate damping of an aircraft by fuzzy and classical PD controller
(2010)Aircraft dynamics are in general nonlinear, time varying, and uncertain. A control system (classical control systems) designed for a flight condition, may not provide the desired stability and performance characteristics ...
