PROVIDING ADJUSTABILITY OF AN AIRCRAFT CONTROL-SYSTEM BY THE METHOD OF ADAPTIVE IDENTIFICATION

Authors
KRUTOVA IN
Citation
In. Krutova, PROVIDING ADJUSTABILITY OF AN AIRCRAFT CONTROL-SYSTEM BY THE METHOD OF ADAPTIVE IDENTIFICATION, Automation and remote control, 57(3), 1996, pp. 385-395
Citations number
10
Categorie Soggetti
Controlo Theory & Cybernetics","Computer Application, Chemistry & Engineering","Instument & Instrumentation","Robotics & Automatic Control
Journal title
Automation and remote control → ACNP
ISSN journal
00051179
Volume
57
Issue
3
Year of publication
1996
Part
2
Pages
385 - 395
Database
ISI
SICI code
0005-1179(1996)57:3<385:PAOAAC>2.0.ZU;2-8
Abstract
Consideration is given to providing adjustability of the system contro lling an aircraft's longitudinal motion by bringing together the outpu ts of the system and reference model through parametric optimization o f the control law. The problem is solved by adaptive identification. C onvergence of the parameter estimates is studied by cluster analysis. Different cases such as linear system and reference model, nonlinear s ystem and reference model, and constrained ranges of the parameters of the control law are discussed.