TsAGI Science Journal
Publicado 6 números por año
ISSN Imprimir: 1948-2590
ISSN En Línea: 1948-2604
ADAPTIVE CONTROL SYSTEM FOR AIRCRAFT LONGITUDINAL MOTION
Volumen 43,
Edición 5, 2012,
pp. 683-695
DOI: 10.1615/TsAGISciJ.2013007158
SINOPSIS
An adaptive algorithm of an aircraft flight control system for longitudinal axis with the use of online identification of moment characteristics is considered. An identification procedure using two "shells" of measurements is proposed. Simulation of longitudinal motion of an aircraft with proposed adaptive system is given.
PALABRAS CLAVE: flight control system, adaptive control, identification of moment characteristics, compensation of aircraft characteristics, model motion
CITADO POR
-
Komar N.N., The Concept of the Aircraft Fault-Tolerant Control Improvement, Upravlâûŝie sistemy i mašiny, 5 (271), 2017. Crossref
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