DocumentCode :
2200126
Title :
Functional feedback in an extremum seeking loop
Author :
Banavar, R.N. ; Chichka, D.F. ; Speyer, J.L.
Volume :
2
fYear :
2001
fDate :
2001
Firstpage :
1316
Abstract :
We analyze the effect of functional feedback in an extremum seeking loop. Our study is motivated by a formation flight problem where the trailing aircraft experiences an outward rolling moment as the vortex effects of the leading aircraft come into play. Viewed as the extremized functional, this rolling moment feeds itself back to the lateral dynamics of the aircraft. In the initial half of the paper we impose restrictions on the curvature of the extremized functional and examine the effect under the assumption of a dynamic time-scale separation between the tracking loops of the linear dynamical system and the extremum seeking loop; in the latter half we remove both these assumptions and instead impose assumed functional forms on the extremized functional
Keywords :
aircraft control; feedback; function approximation; functional equations; linear systems; stability; dynamic time-scale separation; extremum seeking loop; formation flight problem; functional feedback; lateral dynamics; linear dynamical system; outward rolling moment; tracking loops; trailing aircraft; vortex effects; Aerodynamics; Aerospace engineering; Aircraft; Application specific integrated circuits; Control systems; Engines; Feedback loop; Feeds; Measurement; Tracking loops;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 2001. Proceedings of the 40th IEEE Conference on
Conference_Location :
Orlando, FL
Print_ISBN :
0-7803-7061-9
Type :
conf
DOI :
10.1109/.2001.981072
Filename :
981072
Link To Document :
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