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 |
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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 | |
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) |
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Publisher | Elsevier |
Number | 7 |
Volume | 40 |
ISSN (Print) | 1474-6670 |
Conference
Conference | 17th IFAC Symposium on Automatic Control in Aerospace |
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Abbreviated title | ACA' 2007 |
Country/Territory | France |
City | Toulouse |
Period | 25/06/07 → 29/06/07 |
Internet address |