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Flight Parameter Estimation for Augmented Flight Control System Autonomy Airbus

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Cazes, Cazes, author.
Contributor:
Chabert, Marie
Dayre, Rémy
Goupil, Philippe
Le Berre, Hervé
Mailhes, Corinne
Conference Name:
Aerospace Technology Conference & Exposition (2011-10-18 : Toulouse, France)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 2011
Summary:
In the framework of the aircraft global optimization, for future and upcoming programs, current research interests include more Electrical Flight Control System (EFCS) autonomy for a more easy-to-handle aircraft. A possible solution is to increase the number of redundant flight parameter sensors but to the detriment of the aircraft weight and so to the cost and performances. This paper proposes an algorithm using PLS (Partial Least Squares) to estimate a flight parameter from independent sensor measurements. The estimates are then used as so-called "software" or "virtual" sensors, allowing aircraft weight saving. This algorithm is based on an iterative processing and thus can be used in real time in the embedded flight control computer. Furthermore, the resulting flight parameter estimates can be used to detect failures. Different detection strategies are proposed and results show that this method can lead to robust detections
Notes:
Vendor supplied data
Publisher Number:
2011-01-2801
Access Restriction:
Restricted for use by site license

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