TsAGI Science Journal
Выходит 6 номеров в год
ISSN Печать: 1948-2590
ISSN Онлайн: 1948-2604
ADAPTIVE CONTROL SYSTEM FOR AIRCRAFT LONGITUDINAL MOTION
Том 43,
Выпуск 5, 2012,
pp. 683-695
DOI: 10.1615/TsAGISciJ.2013007158
Краткое описание
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.
Ключевые слова: flight control system, adaptive control, identification of moment characteristics, compensation of aircraft characteristics, model motion
ЦИТИРОВАНО В
-
Komar N.N., The Concept of the Aircraft Fault-Tolerant Control Improvement, Upravlâûŝie sistemy i mašiny, 5 (271), 2017. Crossref
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