Designing, Dynamic Modeling and Simulation of ISTECOPTER

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Journal of Aviation
Volume:3 Issue:1
Designing, Dynamic Modeling and Simulation of ISTECOPTER

Designing, Dynamic Modeling and Simulation of ISTECOPTER

Authors : Sezer ÇOBAN, Hasan Hüseyin BİLGİÇ, Tuğrul OKTAY

Pages : 38-44

Doi:10.30518/jav.564376

View : 84 | Download : 8

Publication Date : 2019-06-23

Article Type : Research Paper

Abstract :In this study, İSTECOPTER was modeled, performance evaluations were made and control system was designed . For the control system, lateral, longitudinal and vertical take-off of the UAV insert ignore into journalissuearticles values(Unmanned Aerial Vehicle); and the separate mathematical model of the descent operations were extracted and expressed as the state space model. The mathematical model of the wind distortions that will affect the aircraft during the flight was created and the situation was added to the space model. Proportional Integral Derivative insert ignore into journalissuearticles values(PID); control algorithm was used as a control. The unmanned aircraft was modeled in Solidworks and the simulations in Matlab / Simulink program. the İSTECOPTER is planned to have 4 brushless DC motors and has a weight of approximately 1.5 kg without load and 1 kg of payload is planned. It is planned to enter the TUBITAK rotary wing UAV competition with istecopter which we intend to design and produce.
Keywords : PID, Simulink, UAV Unmanned Aerial Vehicle,

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