Model-Based Solutions for Structural Coupling Problems in Aircraft

S. A. Halsey, R. M. Goodall, B. D. Caldwell, John T. Pearson

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

Abstract

The paper describes a model based approach to provide an integrated structural coupling filter for a military aircraft. It utilises a steady-state version of the well-known Kalman filter, designed using a model containing rigid and flexible modes relevant to longitudinal dynamics, and provides an important alternative to the existing approach using a number of notch filters in the sensor and actuator paths.

Original languageEnglish
Title of host publication17th IFAC Symposium on Automatic Control in Aerospace
PublisherElsevier
Pages503-508
Number of pages6
Volume40
Edition7
ISBN (Print)9783902661241, 9781605607344
DOIs
Publication statusPublished - 2007
Externally publishedYes
Event17th IFAC Symposium on Automatic Control in Aerospace - Toulouse, France
Duration: 25 Jun 200729 Jun 2007
Conference number: 17
https://www.sciencedirect.com/journal/ifac-proceedings-volumes/vol/40/issue/7?page=2

Publication series

NameIFAC Proceedings Volumes (IFAC-PapersOnline)
PublisherElsevier
Number7
Volume40
ISSN (Print)1474-6670

Conference

Conference17th IFAC Symposium on Automatic Control in Aerospace
Abbreviated titleACA' 2007
CountryFrance
CityToulouse
Period25/06/0729/06/07
Internet address

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Cite this

Halsey, S. A., Goodall, R. M., Caldwell, B. D., & Pearson, J. T. (2007). Model-Based Solutions for Structural Coupling Problems in Aircraft. In 17th IFAC Symposium on Automatic Control in Aerospace (7 ed., Vol. 40, pp. 503-508). (IFAC Proceedings Volumes (IFAC-PapersOnline); Vol. 40, No. 7). Elsevier. https://doi.org/10.3182/20070625-5-FR-2916.00086