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
Link To Document :
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