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A comprehensive survey on the methods of angle of attack measurement and estimation in UAVs
- Source :
- Chinese Journal of Aeronautics, Vol 33, Iss 3, Pp 749-770 (2020)
- Publication Year :
- 2020
- Publisher :
- Elsevier, 2020.
-
Abstract
- Angle of Attack (AOA) is a crucial parameter which directly affects the aerodynamic forces of an aircraft. The measurement of AOA is required to ensure a safe flight within its designed flight envelop. This paper intends to summarise a comprehensive survey on the measurement techniques and estimation methods for AOA, specifically in Unmanned Aerial Vehicle (UAV) applications. In the case of UAVs, weight constraint plays a major role as far as sensor suites are concerned. This results in selecting a suitable estimation method to extract AOA using the available data from the autopilot. The most feasible and widely employed AOA measurement technique is by using the Multi-Hole Probes (MHPs). The MHP measures the AOA regarding the pressure variations between the ports. Due to the importance of MHP in AOA measurement, the calibration methods for the MHP are also included in this paper. This paper discusses the AOA measurement using virtual AOA sensors, their importance and the operation. Keywords: Angle of attack estimation, Angle of attack measurement, Angle of attack vane, Five-hole probe, Multi-hole probe, Multi-hole probe calibration, Nine-hole probe, Seven-hole probe, Virtual angle of attack sensor
- Subjects :
- 0209 industrial biotechnology
Angle of attack
Computer science
Mechanical Engineering
Aerospace Engineering
TL1-4050
02 engineering and technology
Weight constraint
01 natural sciences
010305 fluids & plasmas
law.invention
Aerodynamic force
020901 industrial engineering & automation
Control theory
law
0103 physical sciences
Autopilot
Calibration
Estimation methods
Motor vehicles. Aeronautics. Astronautics
Subjects
Details
- Language :
- English
- ISSN :
- 10009361
- Volume :
- 33
- Issue :
- 3
- Database :
- OpenAIRE
- Journal :
- Chinese Journal of Aeronautics
- Accession number :
- edsair.doi.dedup.....cc0d9fd507e6584ad713b02ede2c0938