Record Details

Bifurcation analysis of inertia coupled roll manoeuvres of airplanes

DSpace at IIT Bombay

View Archive Info
 
 
Field Value
 
Title Bifurcation analysis of inertia coupled roll manoeuvres of airplanes
 
Creator SINHA, NK
ANANTHKRISHNAN, N
 
Subject velocity-vector roll
maneuvers
aircraft
jump
bifurcation analysis
constrained manoeuvres
roll performance
transcritical bifurcation
 
Description The extended bifurcation analysis (EBA) technique has been recently proposed for the bifurcation analysis of dynamical systems with constrained equilibrium states. In this paper, the EBA technique is used to investigate non-linear behaviour of an aircraft in constrained roll manoeuvres. A comparative performance analysis of the aircraft in three roll manoeuvres, viz. zero sideslip roll, velocity vector roll, and roll manoeuvre with a linear aileron-rudder interconnect (ARI), has been carried out. Selective numerical simulations are carried out to supplement the information obtained from bifurcation analysis.
 
Publisher PROFESSIONAL ENGINEERING PUBLISHING LTD
 
Date 2011-08-27T07:46:05Z
2011-12-26T12:57:48Z
2011-12-27T05:45:21Z
2011-08-27T07:46:05Z
2011-12-26T12:57:48Z
2011-12-27T05:45:21Z
2003
 
Type Article
 
Identifier PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 217(G2), 75-85
0954-4100
http://dx.doi.org/10.1243/095441003765208736
http://dspace.library.iitb.ac.in/xmlui/handle/10054/11589
http://hdl.handle.net/10054/11589
 
Language en