TsAGI Science Journal
年間 6 号発行
ISSN 印刷: 1948-2590
ISSN オンライン: 1948-2604
ADAPTIVE CONTROL SYSTEM FOR AIRCRAFT LONGITUDINAL MOTION
巻 43,
発行 5, 2012,
pp. 683-695
DOI: 10.1615/TsAGISciJ.2013007158
要約
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.
キーワード: flight control system, adaptive control, identification of moment characteristics, compensation of aircraft characteristics, model motion
によって引用された
-
Komar N.N., The Concept of the Aircraft Fault-Tolerant Control Improvement, Upravlâûŝie sistemy i mašiny, 5 (271), 2017. Crossref
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