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    Performance of Low-Cost Air-Data Sensors for Airspeed and Angle of Attack Measurements in a Flapping-Wing Robot

    Source: Journal of Aerospace Engineering:;2019:;Volume (032):;issue:003
    Author:
    Mohammad Ali Amini;Moosa Ayati
    DOI: doi:10.1061/(ASCE)AS.1943-5525.0000997
    Publisher: American Society of Civil Engineers
    Abstract: Air-data measurements are one of the essential observations for system identification of flapping-wing unmanned aerial vehicles (UAVs). The effects of intensive high-amplitude oscillations of ornithopters on air-data measurements were studied in detail. The movements of an average-sized ornithopter were simulated through a two-degree-of-freedom (2-DOF) mechanism in a wind tunnel, and measurements of an air-data system (pitot and air vane) attached to the mechanism were studied. pitot tests were conducted at different airspeeds and angles of attack (AoAs) using three pitot tubes. The same experimental conditions were created for air-vane measurements. Results revealed that within certain limits, the average measured airspeed was close to the true airspeed values. Two filters were proposed and used for real-time airspeed estimation. Based on the measurements, the oscillation amplitude of the air vane was almost twice that of the real AoA oscillations. However, the mean values of air-vane measurements and real AoAs coincided over one flapping period. For real-time estimation of AoA, which varies very fast with flapping, an estimator based on the least-squares method was implemented.
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      Performance of Low-Cost Air-Data Sensors for Airspeed and Angle of Attack Measurements in a Flapping-Wing Robot

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4256945
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    contributor authorMohammad Ali Amini;Moosa Ayati
    date accessioned2019-06-08T07:23:42Z
    date available2019-06-08T07:23:42Z
    date issued2019
    identifier other%28ASCE%29AS.1943-5525.0000997.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4256945
    description abstractAir-data measurements are one of the essential observations for system identification of flapping-wing unmanned aerial vehicles (UAVs). The effects of intensive high-amplitude oscillations of ornithopters on air-data measurements were studied in detail. The movements of an average-sized ornithopter were simulated through a two-degree-of-freedom (2-DOF) mechanism in a wind tunnel, and measurements of an air-data system (pitot and air vane) attached to the mechanism were studied. pitot tests were conducted at different airspeeds and angles of attack (AoAs) using three pitot tubes. The same experimental conditions were created for air-vane measurements. Results revealed that within certain limits, the average measured airspeed was close to the true airspeed values. Two filters were proposed and used for real-time airspeed estimation. Based on the measurements, the oscillation amplitude of the air vane was almost twice that of the real AoA oscillations. However, the mean values of air-vane measurements and real AoAs coincided over one flapping period. For real-time estimation of AoA, which varies very fast with flapping, an estimator based on the least-squares method was implemented.
    publisherAmerican Society of Civil Engineers
    titlePerformance of Low-Cost Air-Data Sensors for Airspeed and Angle of Attack Measurements in a Flapping-Wing Robot
    typeJournal Article
    journal volume32
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doidoi:10.1061/(ASCE)AS.1943-5525.0000997
    page04019018
    treeJournal of Aerospace Engineering:;2019:;Volume (032):;issue:003
    contenttypeFulltext
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