Flight test of an L 1 adaptive controller on the NASA AirSTAR flight test vehicle

Irene M. Gregory, Enric Xargay, Chengyu Cao, Naira Hovakimyan

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

Abstract

This paper presents results of a flight test of the L 1 adaptive control architecture designed to directly compensate for significant uncertain cross-coupling in nonlinear systems. The flight test was conducted on the subscale turbine powered Generic Transport Model that is an integral part of the Airborne Subscale Transport Aircraft Research system at the NASA Langley Research Center. The results presented are for piloted tasks performed during the flight test.

Original languageEnglish (US)
Title of host publicationAIAA Guidance, Navigation, and Control Conference
DOIs
StatePublished - Dec 1 2010
EventAIAA Guidance, Navigation, and Control Conference - Toronto, ON, Canada
Duration: Aug 2 2010Aug 5 2010

Publication series

NameAIAA Guidance, Navigation, and Control Conference

Other

OtherAIAA Guidance, Navigation, and Control Conference
CountryCanada
CityToronto, ON
Period8/2/108/5/10

ASJC Scopus subject areas

  • Aerospace Engineering
  • Control and Systems Engineering

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  • Cite this

    Gregory, I. M., Xargay, E., Cao, C., & Hovakimyan, N. (2010). Flight test of an L 1 adaptive controller on the NASA AirSTAR flight test vehicle. In AIAA Guidance, Navigation, and Control Conference [AIAA 2010-8015] (AIAA Guidance, Navigation, and Control Conference). https://doi.org/10.2514/6.2010-8015