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Suppression of wing rock of slender delta wings using a single neuron controller

DSpace at IIT Bombay

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Field Value
 
Title Suppression of wing rock of slender delta wings using a single neuron controller
 
Creator JOSHI, SV
SREENATHA, AG
CHANDRASEKHAR, J
 
Subject motion
delta wing
nonlinear
real time
saturation
single neuron
wing rock
 
Description Wing rock is a highly nonlinear phenomenon in which the aircraft undergoes limit cycle roll oscillations at high angles of attack, A single neuron control scheme for suppression of wing rock of slender delta wings is presented. The effectiveness of the control scheme is demonstrated through software simulation and real-time control experiments in a wind tunnel on a 80 degrees swept back, wing, The suppression of the limit cycle is achieved in presence of control saturation, The robustness of the scheme is demonstrated by the suppression of the wing rock at various initial conditions and different angles of attack.
 
Publisher IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
 
Date 2011-08-01T17:22:28Z
2011-12-26T12:53:26Z
2011-12-27T05:39:01Z
2011-08-01T17:22:28Z
2011-12-26T12:53:26Z
2011-12-27T05:39:01Z
1998
 
Type Article
 
Identifier IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 6(5), 671-677
1063-6536
http://dx.doi.org/10.1109/87.709502
http://dspace.library.iitb.ac.in/xmlui/handle/10054/8496
http://hdl.handle.net/10054/8496
 
Language en