Abstract
This paper presents the design features and algorithms of processing the data of a vortex sensor of aerodynamic angle and true air speed aboard a subsonic airplane. This sensor provides measurement of the other altitude-speed flight parameters.
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Soldatkin, V.M., Metody i sredstva izmereniya aerodinamicheskikh uglov letatel’nykh apparatov (Methods and Means for Measuring the Aircraft Aerodynamic Angles), Kazan: Izd. Kazan. Gos. Tekh. Univ., 2001.
Braslavskii, D.A., Logunov, S.S., and Pel’por, D.S., Aviatsionnye pribory i avtomaty (Aeronautical Instruments and Automates), Moscow: Mashinostroenie, 1978.
Soldatkin, V.M. and Soldatkina, E.S., RU Patent 2506596, Byul. Izobr., 2014, no. 4.
Soldatkin, V.M. and Soldatkina, E.M., Vortex Sensor of Aerodynamic Angle and True Airspeed, Izv. Vuz. Av. Tekhnika, 2012, vol. 55, no. 4, pp. 56–59 [Russian Aeronautics (Engl.Transl.). vol. 56, no. 4, pp. 402–407].
Soldatkina, E.S., Analysis of the Metrological Characteristics of the Vortex Sensor of Aerodynamic Angle and True Airspeed, Fundamental’nye i Prikladnye Problemy Tekhniki i Tekhnologii, 2013, no. 2, pp. 111–117.
Soldatkina, E.M., System Engineering Design of a Vortex Aerodynamic Angle and True Airspeed Sensor, Izv. Vuz. Av. Tekhnika, 2013, vol. 56, no. 3, pp. 57–61 [Russian Aeronautics (Engl.Transl.). vol. 56, no. 3, pp. 291–296].
Zalmanzon, L.A., Protochnye elementy pnevmaticheskikh priborov kontrolya i upravleniya (Components for Pneumatic Control Instruments), Moscow: Izd. AN SSSR, 1961.
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Original Russian Text © E.S. Soldatkina, V.M. Soldatkin, 2014, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2014, No. 4, pp. 54–56.
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Soldatkina, E.S., Soldatkin, V.M. Vortex sensor of aerodynamic angle and true airspeed with enhanced functionality. Russ. Aeronaut. 57, 402–405 (2014). https://doi.org/10.3103/S106879981404014X
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DOI: https://doi.org/10.3103/S106879981404014X