Abstract
A systematic design procedure suited to integrate rigid body and aeroelastic control objectives within the mixed sensitivity framework is proposed for a two-degrees-of-freedom control configuration. It is based on a modal representation and combines stability augmentation, structural mode control and maneuver demand in a single linear parameter-varying (LPV) controller. To demonstrate applicability, an integrated flight control system is designed for the nonlinear model of a large flexible aircraft. The integrated controller is shown to greatly reduce structural vibrations while maintaining handling qualities and robustness margins of a conventional controller.
Original language | English (US) |
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Title of host publication | ACC 2015 - 2015 American Control Conference |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
Pages | 3830-3835 |
Number of pages | 6 |
ISBN (Electronic) | 9781479986842 |
DOIs | |
State | Published - Jul 28 2015 |
Event | 2015 American Control Conference, ACC 2015 - Chicago, United States Duration: Jul 1 2015 → Jul 3 2015 |
Publication series
Name | Proceedings of the American Control Conference |
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Volume | 2015-July |
ISSN (Print) | 0743-1619 |
Conference
Conference | 2015 American Control Conference, ACC 2015 |
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Country/Territory | United States |
City | Chicago |
Period | 7/1/15 → 7/3/15 |
Bibliographical note
Publisher Copyright:© 2015 American Automatic Control Council.