Araştırma Makalesi
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Simultaneous Design of a Small UAV (Unmanned Aerial Vehicle) Flight Control System and Lateral State Space Model

Yıl 2018, , 70 - 76, 23.12.2018
https://doi.org/10.30518/jav.461365

Öz

In this study, the design of a
small unmanned aerial vehicle (UAV) and the real-time application of the flight
control system and lateral state-space model were investigated. For this purpose,
an UAV production was carried out, which was assembled from different locations
at certain intervals to the wing and tail set body and moved back and forth
before the flight. An autopilot was then used which allowed the change of P, I,
D values ​​between 1 and 100. First of all, we obtained a lateral state space
model of the UAV and obtained a simulation model of Unmanned Aerial Vehicle. At
the same time, the block diagram of the autopilot system was extracted and
modeled in MATLAB / Simulink environment. Afterwards, SPSA developed a cost
function consisting of ascent, seating time and maximum overrun, and the
Unmanned Aircraft and autopilot system were redesigned simultaneously to
minimize this cost function. High performance is easily observed in simulation
responses and real flights.

Kaynakça

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  • [10] Kuo, B. C. (1963). Analysis and synthesis of sampled-data control systems. Prentice-Hall
  • [11] Ekinci, İ (2016). İnsansız Bir Hava Aracının Yanal Durum Uzay Modelinin ve Uçuş Kontrol Sisteminin Eş Zamanlı Tasarımı. Erciyes Üniversitesi Fen Bilimleri Enstitüsü, Yayımlanmış Yüksek Lisans Tezi, Kayseri
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  • [13] Oktay T., Çoban S. , "Simultaneous Longitudinal and Lateral Flight Control Systems Design For Both Passive and Active Morphing TUAVs ", ELEKTRONİKA IR ELEKTROTECHNİKA, vol.23, no.5, pp.15-20, 2017
Toplam 13 adet kaynakça vardır.

Ayrıntılar

Birincil Dil İngilizce
Konular Uzay Mühendisliği
Bölüm Araştırma Makaleleri
Yazarlar

Sezer Çoban 0000-0001-6750-5001

Tuğrul Oktay

Yayımlanma Tarihi 23 Aralık 2018
Gönderilme Tarihi 19 Eylül 2018
Kabul Tarihi 4 Aralık 2018
Yayımlandığı Sayı Yıl 2018

Kaynak Göster

APA 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. https://doi.org/10.30518/jav.461365

Journal of Aviation - JAV 


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