Controller design for the F-14 pitch axis control problem using the quantitative feedback theory approach

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

Abstract

The controller design of the F-14 pitch axis control problem is examined. The system block diagram is modified by using two, instead of the original four, controllers. The quantitative feedback theory (QFT) is then used to design the robust controllers. Simulations show that the angle-of-attack and pitch rate step responses of the designed system under the linearized plant parameter variations satisfy the design specifications.

Original languageEnglish (US)
Title of host publicationProceedings of the American Control Conference
PublisherPubl by American Automatic Control Council
Pages846-847
Number of pages2
ISBN (Print)0879425652, 9780879425654
DOIs
StatePublished - Jan 1 1991
EventProceedings of the 1991 American Control Conference - Boston, MA, USA
Duration: Jun 26 1991Jun 28 1991

Publication series

NameProceedings of the American Control Conference
Volume1
ISSN (Print)0743-1619

Other

OtherProceedings of the 1991 American Control Conference
CityBoston, MA, USA
Period6/26/916/28/91

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