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
Link To Document :
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