Model-Based Solutions for Structural Coupling Problems in Aircraft

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

doi:10.3182/20070625-5-FR-2916.00086

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 proceeding › Conference contribution › peer-review

2 Citations (Scopus)

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 language	English
Title of host publication	17th IFAC Symposium on Automatic Control in Aerospace
Publisher	Elsevier
Pages	503-508
Number of pages	6
Volume	40
Edition	7
ISBN (Print)	9783902661241, 9781605607344
DOIs	https://doi.org/10.3182/20070625-5-FR-2916.00086
Publication status	Published - 2007
Externally published	Yes
Event	17th IFAC Symposium on Automatic Control in Aerospace - Toulouse, France Duration: 25 Jun 2007 → 29 Jun 2007 Conference number: 17 https://www.sciencedirect.com/journal/ifac-proceedings-volumes/vol/40/issue/7?page=2

Publication series

Name	IFAC Proceedings Volumes (IFAC-PapersOnline)
Publisher	Elsevier
Number	7
Volume	40
ISSN (Print)	1474-6670

Conference

Conference	17th IFAC Symposium on Automatic Control in Aerospace
Abbreviated title	ACA' 2007
Country/Territory	France
City	Toulouse
Period	25/06/07 → 29/06/07
Internet address	https://www.sciencedirect.com/journal/ifac-proceedings-volumes/vol/40/issue/7?page=2

Access to Document

10.3182/20070625-5-FR-2916.00086Licence: Other

Cite this

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title = "Model-Based Solutions for Structural Coupling Problems in Aircraft",

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.",

keywords = "Aeroservoelasticity, Aerospace, Flight control, Kalman filtering, Structural coupling",

author = "Halsey, \{S. A.\} and Goodall, \{R. M.\} and Caldwell, \{B. D.\} and Pearson, \{John T.\}",

year = "2007",

doi = "10.3182/20070625-5-FR-2916.00086",

language = "English",

isbn = "9783902661241",

volume = "40",

series = "IFAC Proceedings Volumes (IFAC-PapersOnline)",

publisher = "Elsevier",

number = "7",

pages = "503--508",

booktitle = "17th IFAC Symposium on Automatic Control in Aerospace",

address = "Netherlands",

edition = "7",

note = "17th IFAC Symposium on Automatic Control in Aerospace, ACA' 2007 ; Conference date: 25-06-2007 Through 29-06-2007",

url = "https://www.sciencedirect.com/journal/ifac-proceedings-volumes/vol/40/issue/7?page=2",

}

Halsey, SA, Goodall, RM, Caldwell, BD & Pearson, JT 2007, Model-Based Solutions for Structural Coupling Problems in Aircraft. in 17th IFAC Symposium on Automatic Control in Aerospace. 7 edn, vol. 40, IFAC Proceedings Volumes (IFAC-PapersOnline), no. 7, vol. 40, Elsevier, pp. 503-508, 17th IFAC Symposium on Automatic Control in Aerospace, Toulouse, France, 25/06/07. https://doi.org/10.3182/20070625-5-FR-2916.00086

Model-Based Solutions for Structural Coupling Problems in Aircraft. / Halsey, S. A.; Goodall, R. M.; Caldwell, B. D. et al.
17th IFAC Symposium on Automatic Control in Aerospace. Vol. 40 7. ed. Elsevier, 2007. p. 503-508 (IFAC Proceedings Volumes (IFAC-PapersOnline); Vol. 40, No. 7).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Model-Based Solutions for Structural Coupling Problems in Aircraft

AU - Halsey, S. A.

AU - Goodall, R. M.

AU - Caldwell, B. D.

AU - Pearson, John T.

N1 - Conference code: 17

PY - 2007

Y1 - 2007

N2 - 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.

AB - 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.

KW - Aeroservoelasticity

KW - Aerospace

KW - Flight control

KW - Kalman filtering

KW - Structural coupling

UR - https://www.scopus.com/pages/publications/79961011775

U2 - 10.3182/20070625-5-FR-2916.00086

DO - 10.3182/20070625-5-FR-2916.00086

M3 - Conference contribution

AN - SCOPUS:79961011775

SN - 9783902661241

SN - 9781605607344

VL - 40

T3 - IFAC Proceedings Volumes (IFAC-PapersOnline)

SP - 503

EP - 508

BT - 17th IFAC Symposium on Automatic Control in Aerospace

PB - Elsevier

T2 - 17th IFAC Symposium on Automatic Control in Aerospace

Y2 - 25 June 2007 through 29 June 2007

ER -

Model-Based Solutions for Structural Coupling Problems in Aircraft

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