Theoretical and Experimental Analysis of Dynamic Model of a Single-Blade Aerial Vehicle Based on Frequency Domain Identification

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تحلیل تئوری و تجربی مدل دینامیکی پرنده تک‌بال بر پایه شناسایی حوزه فرکانس

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Type of Document: M.Sc. Thesis
Language: Farsi
Document No: 50921 (45)
University: Sharif University of Technology
Department: Aerospace Engineering
Advisor(s): Saghafi, Fariborz; Banazadeh, Afshin
Abstract:
The main goal of this work is to estimate the linear transfer function of a single-blade VTOL aerial vehicle, the so-called Monocopter.At first, a prototype of this vehicle is designed and built based on the previously gathered information. The complexity and high manufacturing cost of the first prototype has forced us to build one other simple and cost-effective vehicle. A complete electronic board for data-logging has also designed and built. Many flight test has been carried out and recorded output data are processed by CIFER and MATLAB software in order to identify the dynamic model of the vehicle. The results are presented in different forms
Keywords:
Dynamic Modeling ; Single Bladed Vehicle ; Design and Construction ; Flying Object ; Aerial Vehicles ; Frequency Domain Identification ; Data Acquisition