Control system design for the digitized Grumman F-14 benchmark control problem

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

Abstract

A particular H design approach is coupled with multicriterion optimization to design a pitch axis controller for the F - 14, one of the CSS benchmark control problems. In this two-degree-of-freedom structure, the controller is designed via an H method based on minimizing a weighted quadratic combination of the sensitivity and complementary sensitivity functions of the system. The pre-compensator is used to shape the output responses so as to cause the entire system to achieve the desired performance. The angle-of-attack α(t) model following error, constraints on the normalized pitch rate |q(jΩ)|nom and the effects of the wind gust and sensor noise on α and q are examined. The robustness of α(t) under the aircraft large parameter variations is also studied.

Original languageEnglish (US)
Title of host publicationAmerican Control Conference
Editors Anon
PublisherPubl by IEEE
Pages1113-1117
Number of pages5
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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