scholarly journals Robust control design and testing for an unmanned air vehicle

Author(s):  
R.M. Farhadi ◽  
V.I. Kortunov
2015 ◽  
Vol 220-221 ◽  
pp. 470-478
Author(s):  
Arkadiusz Mystkowski

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.


Automatica ◽  
1996 ◽  
Vol 32 (8) ◽  
pp. 1223-1227 ◽  
Author(s):  
Peter J. Gawthrop ◽  
Richard W. Jones ◽  
Daniel G. Sbarbaro

2002 ◽  
Vol 15 (3-4) ◽  
pp. 285-301 ◽  
Author(s):  
Alberto Herreros ◽  
Enrique Baeyens ◽  
José R. Perán

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