Designing, Dynamic Modeling and Simulation of ISTECOPTER

Year 2019, Volume: 3 Issue: 1, 38 - 44, 23.06.2019

Sezer Çoban Hasan Hüseyin Bilgiç Tuğrul Oktay

https://doi.org/10.30518/jav.564376

Cited By: 5

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
(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.

Keywords

PID, Simulink, UAV(Unmanned Aerial Vehicle)

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