Araştırma Makalesi

Dynamic Modeling and Simulation of Quadcopter for Several Flight Conditions

Sayı: 15 31 Mart 2019
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Dynamic Modeling and Simulation of Quadcopter for Several Flight Conditions

Öz

In this paper, a four-rotor unmanned aerial vehicle was modeled, a control system was designed and performance evaluations were made. For the control system, a separate mathematical model of the unmanned aerial vehicle longitudinal, lateral and vertical take-off and landing operations is omitted and is expressed as a state space model. The mathematical model of the wind disturbances that will affect the unmanned aerial vehicle during the flight was created and the situation was added to the space model. Proportional Integral Derivative (PID) control algorithm was used as the control. Unmanned aerial vehicle modeling was done in Solidworks and simulations were done in Matlab / Simulink program. This paper is one of rare studies that source on quadcopter modeling and control. In the next part of this study, Zankacopter name will be used instead of quadcopter or quadrotor. 

Anahtar Kelimeler

Kaynakça

  1. H. ÇELİK, T. OKTAY, and İ. TÜRKMEN, "İNSANSIZ KÜÇÜK BİR HAVA ARACININ (ZANKA-I) FARKLI TÜRBÜLANS ORTAMLARINDA MODEL ÖNGÖRÜLÜ KONTROLÜ VE GÜRBÜZLÜK TESTİ," Journal of Aeronautics & Space Technologies/Havacilik ve Uzay Teknolojileri Dergisi, vol. 9, 2016.
  2. R. Austin, Unmanned aircraft systems: UAVS design, development and deployment vol. 54: John Wiley & Sons, 2011.
  3. G. Hoffmann, D. G. Rajnarayan, S. L. Waslander, D. Dostal, J. S. Jang, and C. J. Tomlin, "The Stanford testbed of autonomous rotorcraft for multi agent control (STARMAC)," in Digital Avionics Systems Conference, 2004. DASC 04. The 23rd, 2004, pp. 12. E. 4-121.
  4. J. P. How, B. BEHIHKE, A. Frank, D. Dale, and J. Vian, "Real-time indoor autonomous vehicle test environment," IEEE control systems, vol. 28, pp. 51-64, 2008.
  5. F. Šolc, "Modelling and Control of a Quadrocopter," Advanced in Military Technology, vol. 1, pp. 29-38, 2007.
  6. M. Prabha, R. Thottungal, and S. Kaliappan, "Modeling and Simulation of X-Zankacopter Control," International Journal for Research in Applied Science & Engineering Technology (IJRASET).[online] Available at: http://www. ijraset. com/fileserve. php, 2016.
  7. J. Wang, S. Xin, and Y. Zhang, "Modeling and Control of a Zankacopter Vehicle Subject to Disturbance Load," 2017.
  8. G. Ononiwu, O. Onojo, O. Ozioko, and O. Nosiri, "Zankacopter Design for Payload Delivery," Journal of Computer and Communications, vol. 4, pp. 1-12, 2016.

Ayrıntılar

Birincil Dil

İngilizce

Konular

Mühendislik

Bölüm

Araştırma Makalesi

Yayımlanma Tarihi

31 Mart 2019

Gönderilme Tarihi

3 Ocak 2019

Kabul Tarihi

2 Mart 2019

Yayımlandığı Sayı

Yıl 2019 Sayı: 15

Kaynak Göster

APA
Oktay, T., & Köse, O. (2019). Dynamic Modeling and Simulation of Quadcopter for Several Flight Conditions. Avrupa Bilim ve Teknoloji Dergisi, 15, 132-142. https://doi.org/10.31590/ejosat.507222
AMA
1.Oktay T, Köse O. Dynamic Modeling and Simulation of Quadcopter for Several Flight Conditions. EJOSAT. 2019;(15):132-142. doi:10.31590/ejosat.507222
Chicago
Oktay, Tuğrul, ve Oğuz Köse. 2019. “Dynamic Modeling and Simulation of Quadcopter for Several Flight Conditions”. Avrupa Bilim ve Teknoloji Dergisi, sy 15: 132-42. https://doi.org/10.31590/ejosat.507222.
EndNote
Oktay T, Köse O (01 Mart 2019) Dynamic Modeling and Simulation of Quadcopter for Several Flight Conditions. Avrupa Bilim ve Teknoloji Dergisi 15 132–142.
IEEE
[1]T. Oktay ve O. Köse, “Dynamic Modeling and Simulation of Quadcopter for Several Flight Conditions”, EJOSAT, sy 15, ss. 132–142, Mar. 2019, doi: 10.31590/ejosat.507222.
ISNAD
Oktay, Tuğrul - Köse, Oğuz. “Dynamic Modeling and Simulation of Quadcopter for Several Flight Conditions”. Avrupa Bilim ve Teknoloji Dergisi. 15 (01 Mart 2019): 132-142. https://doi.org/10.31590/ejosat.507222.
JAMA
1.Oktay T, Köse O. Dynamic Modeling and Simulation of Quadcopter for Several Flight Conditions. EJOSAT. 2019;:132–142.
MLA
Oktay, Tuğrul, ve Oğuz Köse. “Dynamic Modeling and Simulation of Quadcopter for Several Flight Conditions”. Avrupa Bilim ve Teknoloji Dergisi, sy 15, Mart 2019, ss. 132-4, doi:10.31590/ejosat.507222.
Vancouver
1.Tuğrul Oktay, Oğuz Köse. Dynamic Modeling and Simulation of Quadcopter for Several Flight Conditions. EJOSAT. 01 Mart 2019;(15):132-4. doi:10.31590/ejosat.507222

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