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Characterization and selection of basic parameters for steering servo of a small remotely-piloted single-rotor helicopter with tail rotor

  • Flight Dynamics and Control of Flight Vehicles
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Abstract

The basic parameters of steering servo for a small remotely piloted single-rotor helicopter with tail rotor are determined.

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References

  1. Novoselov, A.S., Bolnokin, V.E., Chinaev, P.I., and Yur’ev, A.N., Sistemy adaptivnogo upravleniya letatel’nymi apparatami (Aircraft Adaptive Control Systems), Moscow: Mashinostroenie, 1987.

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Authors and Affiliations

  1. Moscow Aviation Institute (National Research University), Volokolamskoe shosse 4, Moscow, 125993, Russia

    D. A. D’yakonov, O. A. Zavalov, D. A. Kuptsov & I. K. Turkin

Authors
  1. D. A. D’yakonov
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  2. O. A. Zavalov
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  3. D. A. Kuptsov
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  4. I. K. Turkin
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Corresponding author

Correspondence to D. A. D’yakonov.

Additional information

Original Russian Text © D.A. D’yakonov, O.A. Zavalov, D.A. Kuptsov, I.K. Turkin, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2014, No. 4, pp. 17–19.

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D’yakonov, D.A., Zavalov, O.A., Kuptsov, D.A. et al. Characterization and selection of basic parameters for steering servo of a small remotely-piloted single-rotor helicopter with tail rotor. Russ. Aeronaut. 57, 349–352 (2014). https://doi.org/10.3103/S1068799814040059

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  • DOI: https://doi.org/10.3103/S1068799814040059

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