DocumentCode
1813176
Title
Peak-seeking control with application to formation flight
Author
Chichka, D.F. ; Speyer, J.L. ; Park, C.G.
Author_Institution
California Univ., Los Angeles, CA, USA
Volume
3
fYear
1999
fDate
1999
Firstpage
2463
Abstract
A new controller is proposed for linear systems with unknown optimal operating points. It is assumed that the desired operating point represents the maximum of a function of the states of the system. The controller uses a modified Kalman filter to estimate the derivatives of this function, and the controller drives the system to the optimum. The controller is derived in the context of the formation flight of aircraft for drag reduction, and a simulation is used to provide preliminary results
Keywords
Kalman filters; aircraft control; linear systems; optimal control; state estimation; Kalman filter; aircraft control; formation flight; linear systems; peak-seeking control; state estimation; Adaptive control; Aerodynamics; Aerospace control; Aerospace simulation; Aircraft; Context modeling; Control systems; Linear systems; Optimal control; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1999. Proceedings of the 38th IEEE Conference on
Conference_Location
Phoenix, AZ
ISSN
0191-2216
Print_ISBN
0-7803-5250-5
Type
conf
DOI
10.1109/CDC.1999.831295
Filename
831295
Link To Document