DocumentCode
1751587
Title
A velocity-based framework for the robust stability analysis of dynamic inversion flight controllers
Author
Tsourdos, A. ; Leith, D.J. ; Leithead, W.E. ; White, B.A.
Author_Institution
Dept. of Aerospace, Power & Sensors, Cranfield Univ.-RMCS, UK
Volume
5
fYear
2001
fDate
2001
Firstpage
3341
Abstract
Methods for analysing the robustness of linear systems to parametric uncertainty are relatively well developed. However, the converse is true for nonlinear systems. The recently developed velocity-based framework provides a degree of continuity with linear methods which has the potential to allow established linear methods to be applied when analysing the robustness of nonlinear systems to uncertainty. This paper reports initial investigations in this area with particular reference to the guided weapons application area
Keywords
control system analysis; missile guidance; nonlinear control systems; robust control; uncertain systems; dynamic inversion flight controllers; guided missiles; guided weapons; nonlinear systems; parametric uncertainty; robust stability analysis; robustness analysis; velocity-based framework; Aerodynamics; Linear systems; Nonlinear dynamical systems; Nonlinear systems; Robust control; Robust stability; Robustness; Uncertainty; Vehicle dynamics; Velocity control;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2001. Proceedings of the 2001
Conference_Location
Arlington, VA
ISSN
0743-1619
Print_ISBN
0-7803-6495-3
Type
conf
DOI
10.1109/ACC.2001.946144
Filename
946144
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