ROBUST CONTROL DESIGN TO SUPPRESS WING ROCK MOTION OF A WIND-TUNNEL AIRCRAFT MODEL IN 3DOF GIMBALS

2014 ◽  
Vol 45 (8) ◽  
pp. 977-992 ◽  
Author(s):  
Maria Evguenievna Sidoryuk
Author(s):  
D. I. Ignatyev

High-angles-of-attack dynamics of aircraft are complicated with dangerous phenomena such as wing rock, stall, and spin. Autonomous dynamically scaled aircraft model mounted in three-degree-of-freedom (3DoF) dynamic rig is proposed for studying aircraft dynamics and prototyping of control laws in wind tunnel. Dynamics of the scaled aircraft model in 3DoF manoeuvre rig in wind tunnel is considered. The model limit-cycle oscillations are obtained at high angles of attack. A neural network (NN) adaptive control suppressing wing rock motion is designed. The wing rock suppression with the proposed control law is validated using nonlinear time-domain simulations.


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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