Design examples: Adaptive tracking control in the presence of input constraints for a fighter aircraft and a generic missile

Amir Ajami, Naira Hovakimyan, Eugene Lavretsky

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

Abstract

Two flight control related examples of adaptive autopilot design in the presence of actuator constraints are presented. The demonstrated methodology maintains closed-loop stability by changing guidance commands on-line. In addition, the method is capable of avoiding control saturation at all times, if required.

Original languageEnglish (US)
Title of host publicationCollection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2005
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
Pages5916-5924
Number of pages9
ISBN (Print)1563477378, 9781563477379
DOIs
StatePublished - Jan 1 2005
Externally publishedYes
EventAIAA Guidance, Navigation, and Control Conference 2005 - San Francisco, CA, United States
Duration: Aug 15 2005Aug 18 2005

Publication series

NameCollection of Technical Papers - AIAA Guidance, Navigation, and Control Conference
Volume8

Other

OtherAIAA Guidance, Navigation, and Control Conference 2005
CountryUnited States
CitySan Francisco, CA
Period8/15/058/18/05

ASJC Scopus subject areas

  • Engineering(all)

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  • Cite this

    Ajami, A., Hovakimyan, N., & Lavretsky, E. (2005). Design examples: Adaptive tracking control in the presence of input constraints for a fighter aircraft and a generic missile. In Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2005 (pp. 5916-5924). (Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference; Vol. 8). American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.2005-6444