Model Identification of a Micro Air Vehicle in Loitering Flight Based on Attitude Performance Evaluation

2004 ◽  
Vol 20 (4) ◽  
pp. 702-712 ◽  
Author(s):  
H. Wu ◽  
D. Sun ◽  
Z. Zhou
Keyword(s):  
Performance Evaluation ◽  
Model Identification ◽  
Micro Air Vehicle ◽  
Air Vehicle

SISO Model Identification of a Micro Air Vehicle for Robust Control Design

2015 ◽  
Vol 220-221 ◽  
pp. 470-478
Author(s):  
Arkadiusz Mystkowski
Keyword(s):  
Robust Control ◽  
Delta Wing ◽  
Angular Rate ◽  
Model Identification ◽  
Control Design ◽  
Real Data ◽  
Micro Air Vehicle ◽  
Lateral Direction ◽  
Air Vehicle ◽  
Robust Control Design

This paper describes a model identification method of a Micro Air Vehicle (MAV) for a further purpose of the robust control design. The identification procedure is based on logged real data collected from flight tests. For the identification purpose, both frequency and time-domain techniques are used. Identification results are presented for the lateral direction dynamics using the elevon (aileron deflection) as input and the roll angular rate as output. The MAV is a single-delta wing of the 0.84 m wingspan and 1.2 kg of total mass (ready to flight). The main goal of the system identification process is to achieve the best possible fit between the raw data and a dynamic model which is called a nominal model.

scholarly journals Model identification of a Micro Air Vehicle

2007 ◽  
Vol 4 (4) ◽  
pp. 227-236 ◽  
Author(s):  
Jorge Niño ◽  
Flavius Mitrache ◽  
Peter Cosyn ◽  
Robin De Keyser
Keyword(s):  
Model Identification ◽  
Micro Air Vehicle ◽  
Air Vehicle

Design and Fabrication of an SU-8 Biomimetic Flapping-wing Micro Air Vehicle by MEMS Technology

ROBOT ◽  
2011 ◽  
Vol 33 (3) ◽  
pp. 366-370 ◽  
Author(s):  
Pengcheng CHI ◽  
Weiping ZHANG ◽  
Wenyuan CHEN ◽  
Hongyi LI ◽  
Kun MENG ◽  
...  
Keyword(s):  
Flapping Wing ◽  
Micro Air Vehicle ◽  
Air Vehicle ◽  
Mems Technology
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