DocumentCode
3158316
Title
Development of alpha sensor for unmanned aerial systems
Author
Park, Mi-Hyun ; Kim, Sung-Su ; Ryoo, Chang-Kyung ; Choi, Keeyoung ; Park, Choonbae
Author_Institution
Dept. of Aerosp. Eng., Inha Univ., Incheon
fYear
2008
fDate
20-22 Aug. 2008
Firstpage
2131
Lastpage
2134
Abstract
An alpha sensor implies an angle of attack sensor to measure the angle between the aircraftpsilas reference line and the relative wind vector to the aircraft. Accurate measurements of AOA (angle-of-attack) are important to identify the aerodynamic coefficients and to evaluate the flight performance of an UAS. For a small scale UAS, AOA is usually estimated by AHRS (attitude heading reference system) combined with an GPS receiver, but this method provides poor information in general. In this paper, a null type alpha sensor developed by aerospace control and system Lab. in Inha University is introduced. The null type alpha sensor has many advantages compared with other kinds of alpha sensors. Most of all it has uniform error characteristics against AOA. And, as the speed increases, the sensor provides more accurate measurements.
Keywords
aerodynamics; aerospace robotics; remotely operated vehicles; sensors; GPS receiver; aerodynamic coefficients; aircraft reference line; angle-of-attack; attack sensors; attitude heading reference system; flight performance; null type alpha sensor; unmanned aerial systems; Aerodynamics; Aircraft propulsion; Blades; Electromechanical sensors; Goniometers; Laboratories; Probes; Sensor phenomena and characterization; Sensor systems; Temperature sensors; Alpha sensor; angle of attack; differential pressure; null type;
fLanguage
English
Publisher
ieee
Conference_Titel
SICE Annual Conference, 2008
Conference_Location
Tokyo
Print_ISBN
978-4-907764-30-2
Electronic_ISBN
978-4-907764-29-6
Type
conf
DOI
10.1109/SICE.2008.4655015
Filename
4655015
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