Research Article
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Designing, Dynamic Modeling and Simulation of ISTECOPTER

Year 2019, , 38 - 44, 23.06.2019
https://doi.org/10.30518/jav.564376

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.

References

  • [1] A. Marks, J. F. Whidborne, and I. Yamamoto, "Control allocation for fault tolerant control of a VTOL octorotor," in Control (CONTROL), 2012 UKACC International Conference on, 2012, pp. 357-362.
  • [2] G. Staples, "Propeller Static & Dynamic Thrust Calculation," ed, 2015.
  • [3] S. Bouabdallah, P. Murrieri, and R. Siegwart, "Design and control of an indoor micro zankacopter," in Robotics and Automation, 2004. Proceedings. ICRA'04. 2004 IEEE International Conference on, 2004, pp. 4393-4398.
  • [4] T. Oktay and S. Coban, "Simultaneous Longitudinal and Lateral Flight Control Systems Design for Both Passive and Active Morphing TUAVs," Elektronika ir Elektrotechnika, vol. 23, pp. 15-20, 2017.
  • [5] P. Akyol, "Dısturbance rejectıon and attıtude control of zankacopter wıth log," Başkent Üniversitesi Fen Bilimleri Enstitüsü, 2017.
  • [6] B. L. Stevens, F. L. Lewis, and E. N. Johnson, Aircraft control and simulation: dynamics, controls design, and autonomous systems: John Wiley & Sons, 2015.
  • [7] Çoban, S . (2018). Variance Constrained Vibration Control of Morphing Tactical Unmanned Aerial Vehicles (TUAVs). Avrupa Bilim ve Teknoloji Dergisi, (14), 269-271. DOI: 10.31590/ejosat.475870
  • [8] ÇOBAN, S , OKTAY, T . (2018). Simultaneous Design of a Small UAV (Unmanned Aerial Vehicle) Flight Control System and Lateral State Space Model. Journal of Aviation, 2 (2), 70-76. DOI: 10.30518/jav.461365
  • [9] K. Alexis, G. Nikolakopoulos, and A. Tzes, "Constrained-control of a zankacopter helicopter for trajectory tracking under wind-gust disturbances," in MELECON 2010-2010 15th IEEE Mediterranean Electrotechnical Conference, 2010, pp. 1411-1416.
  • [10] Oktay, T , Köse, O . (2019). Dynamic Modeling and Simulation of Quadcopter for Several Flight Conditions. Avrupa Bilim ve Teknoloji Dergisi, (15), 132-142. DOI: 10.31590/ejosat.507222
Year 2019, , 38 - 44, 23.06.2019
https://doi.org/10.30518/jav.564376

Abstract

References

  • [1] A. Marks, J. F. Whidborne, and I. Yamamoto, "Control allocation for fault tolerant control of a VTOL octorotor," in Control (CONTROL), 2012 UKACC International Conference on, 2012, pp. 357-362.
  • [2] G. Staples, "Propeller Static & Dynamic Thrust Calculation," ed, 2015.
  • [3] S. Bouabdallah, P. Murrieri, and R. Siegwart, "Design and control of an indoor micro zankacopter," in Robotics and Automation, 2004. Proceedings. ICRA'04. 2004 IEEE International Conference on, 2004, pp. 4393-4398.
  • [4] T. Oktay and S. Coban, "Simultaneous Longitudinal and Lateral Flight Control Systems Design for Both Passive and Active Morphing TUAVs," Elektronika ir Elektrotechnika, vol. 23, pp. 15-20, 2017.
  • [5] P. Akyol, "Dısturbance rejectıon and attıtude control of zankacopter wıth log," Başkent Üniversitesi Fen Bilimleri Enstitüsü, 2017.
  • [6] B. L. Stevens, F. L. Lewis, and E. N. Johnson, Aircraft control and simulation: dynamics, controls design, and autonomous systems: John Wiley & Sons, 2015.
  • [7] Çoban, S . (2018). Variance Constrained Vibration Control of Morphing Tactical Unmanned Aerial Vehicles (TUAVs). Avrupa Bilim ve Teknoloji Dergisi, (14), 269-271. DOI: 10.31590/ejosat.475870
  • [8] ÇOBAN, S , OKTAY, T . (2018). Simultaneous Design of a Small UAV (Unmanned Aerial Vehicle) Flight Control System and Lateral State Space Model. Journal of Aviation, 2 (2), 70-76. DOI: 10.30518/jav.461365
  • [9] K. Alexis, G. Nikolakopoulos, and A. Tzes, "Constrained-control of a zankacopter helicopter for trajectory tracking under wind-gust disturbances," in MELECON 2010-2010 15th IEEE Mediterranean Electrotechnical Conference, 2010, pp. 1411-1416.
  • [10] Oktay, T , Köse, O . (2019). Dynamic Modeling and Simulation of Quadcopter for Several Flight Conditions. Avrupa Bilim ve Teknoloji Dergisi, (15), 132-142. DOI: 10.31590/ejosat.507222
There are 10 citations in total.

Details

Primary Language English
Subjects Aerospace Engineering
Journal Section Research Articles
Authors

Sezer Çoban 0000-0001-6750-5001

Hasan Hüseyin Bilgiç 0000-0001-6006-8056

Tuğrul Oktay 0000-0003-4860-2230

Publication Date June 23, 2019
Submission Date May 13, 2019
Acceptance Date June 24, 2019
Published in Issue Year 2019

Cite

APA Çoban, S., Bilgiç, H. H., & Oktay, T. (2019). Designing, Dynamic Modeling and Simulation of ISTECOPTER. Journal of Aviation, 3(1), 38-44. https://doi.org/10.30518/jav.564376

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