Abstract
Structural coupling is the disturbance to the aircraft's inertial sensors caused by the flexibility in the airframe, and is particularly problematic for modern combat aircraft. The current solution uses a series of notch filters to remove the structural frequencies, but these introduce significant phase delays into the control loop. This paper presents some experimental and theoretical results from a flexible beam, and the use of Kalman filters to reduce the effects of structural coupling. This work is part of an ongoing project in conjunction with BAE Systems.
| Original language | English |
|---|---|
| Title of host publication | Proceedings of the 15th IFAC World Congress, International Federation of Automatic Control |
| Publisher | Elsevier |
| Pages | 253-258 |
| Number of pages | 6 |
| Volume | 35 |
| Edition | 1 |
| ISBN (Print) | 9783902661746 |
| DOIs | |
| Publication status | Published - 2002 |
| Externally published | Yes |
| Event | 15th World Congress of the International Federation of Automatic Control - Barcelona, Spain Duration: 21 Jul 2002 → 26 Jul 2002 Conference number: 15 https://www.sciencedirect.com/journal/ifac-proceedings-volumes/vol/35/issue/1 |
Publication series
| Name | IFAC Proceedings Volumes (IFAC-PapersOnline) |
|---|---|
| Publisher | Elsevier |
| Number | 1 |
| Volume | 35 |
| ISSN (Print) | 1474-6670 |
Conference
| Conference | 15th World Congress of the International Federation of Automatic Control |
|---|---|
| Country/Territory | Spain |
| City | Barcelona |
| Period | 21/07/02 → 26/07/02 |
| Internet address |
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