Design of a robust dynamic inversion lateral/directional flight controller

Sadok Hougui, Gary J. Balas, William L. Garrard

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

4 Scopus citations

Abstract

In this paper dynamic inversion and structured singular value (μ) techniques are applied to the design of lateral/directional controllers for a high performance aircraft. The controllers are designed to achieve specified handling qualities with robustness to modeling errors.

Original languageEnglish (US)
Title of host publicationGuidance, Navigation, and Control Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
Pages738-749
Number of pages12
StatePublished - Jan 1 1995
EventGuidance, Navigation, and Control Conference, 1995 - Baltimore, United States
Duration: Aug 7 1995Aug 10 1995

Other

OtherGuidance, Navigation, and Control Conference, 1995
CountryUnited States
CityBaltimore
Period8/7/958/10/95

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  • Cite this

    Hougui, S., Balas, G. J., & Garrard, W. L. (1995). Design of a robust dynamic inversion lateral/directional flight controller. In Guidance, Navigation, and Control Conference (pp. 738-749). American Institute of Aeronautics and Astronautics Inc, AIAA.