TsAGI Science Journal
Publicou 6 edições por ano
ISSN Imprimir: 1948-2590
ISSN On-line: 1948-2604
ADAPTIVE CONTROL SYSTEM FOR AIRCRAFT LONGITUDINAL MOTION
Volume 43,
Edição 5, 2012,
pp. 683-695
DOI: 10.1615/TsAGISciJ.2013007158
RESUMO
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.
Palavras-chave: flight control system, adaptive control, identification of moment characteristics, compensation of aircraft characteristics, model motion
CITADO POR
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Komar N.N., The Concept of the Aircraft Fault-Tolerant Control Improvement, Upravlâûŝie sistemy i mašiny, 5 (271), 2017. Crossref
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