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Panoramic Sensor of the Aerodynamic Angle and True Airspeed with the Fixed Receiver and Ultrasonic Instrumentation Channels

  • AIRCRAFT INSTRUMENTS AND INSTRUMENTATION COMPUTER COMPLEXES
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Abstract

The functional diagram is given, analytical models of processing and determining of the aerodynamic angle and true airspeed of the panoramic sensor with the fixed receiver of incident flow and ultrasonic instrumentation channels are disclosed. The competitive advantages and prospects of using the original panoramic sensor of the aerodynamic angle and true airspeed with ultrasonic instrumentation channels on small-sized manned and unmanned aircraft vehicles are revealed.

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Authors and Affiliations

  1. Tupolev Kazan National Research Technical University, ul. Karla Marksa 10, 420111, Kazan, Tatarstan, Russia

    V. V. Soldatkin, V. M. Soldatkin, E. S. Efremova & A. V. Nikitin

Authors
  1. V. V. Soldatkin
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  2. V. M. Soldatkin
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  3. E. S. Efremova
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  4. A. V. Nikitin
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Corresponding author

Correspondence to V. V. Soldatkin.

Additional information

Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2021, No. 3, pp. 153 - 159.

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Soldatkin, V.V., Soldatkin, V.M., Efremova, E.S. et al. Panoramic Sensor of the Aerodynamic Angle and True Airspeed with the Fixed Receiver and Ultrasonic Instrumentation Channels. Russ. Aeronaut. 64, 526–532 (2021). https://doi.org/10.3103/S1068799821030211

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  • DOI: https://doi.org/10.3103/S1068799821030211

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