Application of a z-plane design method to the Grumman F-14 pitch axis control problem

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

Abstract

A specific z-plane control design technique is used to design the pitch axis controller for the Grumman F-14 aircraft. Simulations show that the angle-of-attack (sampled-data) step response of the system satisfies the design specifications. Due to the sampling, a non-minimum phase zero is induced in the plant which makes the controller unstable. An attempt is also taken to stabilize the controller via the H model-matching technique.

Original languageEnglish (US)
Title of host publicationAmerican Control Conference
Editors Anon
PublisherPubl by IEEE
Pages1111-1112
Number of pages2
ISBN (Print)0780308611
StatePublished - Dec 1 1993
EventProceedings of the 1993 American Control Conference Part 3 (of 3) - San Francisco, CA, USA
Duration: Jun 2 1993Jun 4 1993

Publication series

NameAmerican Control Conference

Other

OtherProceedings of the 1993 American Control Conference Part 3 (of 3)
CitySan Francisco, CA, USA
Period6/2/936/4/93

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