Flight Dynamics Analysis of a High Aspect Ratio Wing UAV
Publish Year: 1396
نوع سند: مقاله کنفرانسی
زبان: English
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شناسه ملی سند علمی:
MECHAERO02_300
تاریخ نمایه سازی: 13 شهریور 1396
Abstract:
In this paper flight dynamics of a UAV with high aspect ratio wing has been simulated. Mean axis theory was the base of simulation and flight dynamics and vibration equations have been coupled through interaction of aerodynamic loads. Mode shapes of the structure has been extracted by software and introduced to the equations. Response to step deflection of elevator has been simulated and a comparison has been made with rigid vehicle.
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Authors
Javad Masrour
Aeospace Complea,Malek Ashtar University, Tehran, Iran
S. Hossein Sadati
Aeospace Complea,Malek Ashtar University, Tehran, Iran
Morteza Shahravi
Aeospace Complea,Malek Ashtar University, Tehran, Iran