Yayınlanmış 1 Ocak 2012
| Sürüm v1
Dergi makalesi
Açık
Mathematical modeling and vertical flight control of a tilt-wing UAV
Oluşturanlar
- 1. Sabanci Univ, Fac Engn & Nat Sci, TR-34956 Istanbul, Turkey
- 2. YTU, Elect & Elect Engn Fac, TR-34349 Istanbul, Turkey
- 3. Gebze Inst Technol GYTE, Fac Engn, TR-41400 Cayirova Gebze, Kocaeli, Turkey
Açıklama
This paper presents a mathematical model and vertical flight control algorithms for a new tilt-wing unmanned aerial vehicle (UAV). The vehicle is capable of vertical take-off and landing (VTOL). Due to its tilt-wing structure, it can also fly horizontally. The mathematical model of the vehicle is obtained using Newton-Euler formulation. A gravity compensated PID controller is designed for altitude control, and three PID controllers are designed for attitude stabilization of the vehicle. Performances of these controllers are found to be quite satisfactory as demonstrated by indoor and outdoor flight experiments.
Dosyalar
10-3906-elk-1007-624.pdf
Dosyalar
(997.4 kB)
| Ad | Boyut | Hepisini indir |
|---|---|---|
|
md5:28de340727c831b69bbfeb838a3c4721
|
997.4 kB | Ön İzleme İndir |