Implementation of the Rauch-Tung-Striebel Smoother for Sensor Compatibility Correction of a Fixed-Wing Unmanned Air Vehicle

This paper presents a complete procedure for sensor compatibility correction of a fixed-wing Unmanned Air Vehicle (UAV). The sensors consist of a differential air pressure transducer for airspeed measurement, two airdata vanes installed on an airdata probe for angle of attack (AoA) and angle of side...

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Bibliographic Details
Main Authors: Fei-Bin Hsiao, Woei-Leong Chan
Format: Article
Language:English
Published: MDPI AG 2011-03-01
Series:Sensors
Subjects:
Online Access:http://www.mdpi.com/1424-8220/11/4/3738/