Application of ℒ1 adaptive controller to wing rock

Chengyu Cao, Naira Hovakimyan, Eugene Lavretsky

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Wing rock is one of the well known instabilities that occurs in aircraft dynamics at moderate to high angles of attack. Therefore it serves as a classical benchmark example for demonstration of various control methodologies. In this paper, we present application of a novel ℒ1 adaptive control architecture to wing rock that ensures smooth transient behavior for system's both signals, control and output simultaneously, in addition to the asymptotic tracking.

Original languageEnglish (US)
Title of host publicationCollection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2006
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
Pages2941-2952
Number of pages12
ISBN (Print)1563478196, 9781563478192
DOIs
StatePublished - 2006
Externally publishedYes
EventAIAA Guidance, Navigation, and Control Conference 2006 - Keystone, CO, United States
Duration: Aug 21 2006Aug 24 2006

Publication series

NameCollection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2006
Volume5

Other

OtherAIAA Guidance, Navigation, and Control Conference 2006
CountryUnited States
CityKeystone, CO
Period8/21/068/24/06

ASJC Scopus subject areas

  • Engineering(all)

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