Record Details

DESIGN OF A ROBUST CONTROLLER FOR A SUPERSONIC AIRCRAFT USING H-INFINITY APPROACH

DSpace at IIT Bombay

View Archive Info
 
 
Field Value
 
Title DESIGN OF A ROBUST CONTROLLER FOR A SUPERSONIC AIRCRAFT USING H-INFINITY APPROACH
 
Creator ATHANI, VV
AGARWAL, S
 
Subject model
flight control
h-infinity control
robust control
model reference control
mixed sensitivity design
loop-shaping design
 
Description In this paper an H(infinity) optimal, robust flight control system design for a supersonic aircraft has been described. Separate controllers are designed for longitudinal and lateral motions. A general two-degrees-of-freedom controller is proposed, where feedback control is designed for robust performance augmentation, while a series compensator is used to ensure the requisite handling qualities. Three alternative methods to achieve performance robustness have been discussed. The results obtained are very encouraging. It is hoped that this approach will equip the flight control engineers with an alternative to the conventional methods.
 
Publisher PERGAMON-ELSEVIER SCIENCE LTD
 
Date 2011-08-24T00:10:50Z
2011-12-26T12:56:40Z
2011-12-27T05:45:43Z
2011-08-24T00:10:50Z
2011-12-26T12:56:40Z
2011-12-27T05:45:43Z
1994
 
Type Article
 
Identifier CONTROL ENGINEERING PRACTICE, 2(6), 1051-1061
0967-0661
http://dx.doi.org/10.1016/0967-0661(94)91627-6
http://dspace.library.iitb.ac.in/xmlui/handle/10054/10697
http://hdl.handle.net/10054/10697
 
Language en