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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 (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 (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.
Çoban et al. (Wed,) studied this question.