Designing, Dynamic Modeling and Simulation of ISTECOPTER
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
References
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Details
Primary Language
English
Subjects
Aerospace Engineering
Journal Section
Research Article
Authors
Sezer Çoban
*
0000-0001-6750-5001
Türkiye
Publication Date
June 23, 2019
Submission Date
May 13, 2019
Acceptance Date
June 24, 2019
Published in Issue
Year 2019 Volume: 3 Number: 1
Cited By
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