Title :
Adaptive control laws for F-8 flight test
Author :
Stein, G. ; Hartmann, G.L. ; Hendrick, R.C.
Author_Institution :
Honeywell Inc., Minneapolis, Minnesota
Abstract :
This paper presents design and performance details for a set of adaptive flight control laws to be flight-tested in NASA´s F-8 digital fly-by-wire research aircraft. These control laws implement an explicit maximum likelihood identification algorithm to estimate key aircraft parameters. The parameter estimates are then used to compute gains in a quadraticoptimal command augmentation control law.
Keywords :
Adaptive control; Adaptive systems; Aerospace control; Aircraft; Equations; Maximum likelihood estimation; Parameter estimation; Processor scheduling; Programmable control; Testing;
Conference_Titel :
Decision and Control including the 14th Symposium on Adaptive Processes, 1975 IEEE Conference on
Conference_Location :
Houston, TX, USA
DOI :
10.1109/CDC.1975.270682
