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Method and calculation of basic parameters of different types of control servoactuators using minimal installed power criterion

  • Control Systems of Moving Objects
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Journal of Computer and Systems Sciences International Aims and scope

Abstract

Problems of choice of the type of a control servoactuator of the aircraft by minimal installed power criterion are considered based on the methodology and algorithms of parametric synthesis of different types of servoactuators. The most rational solution for a maneuvering aircraft is determined from calculations; future implementation of the best variant at PC RAC “MIG” is possible.

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References

  1. Proceedings of 25th Congress of the International Council of the Sciences ICAS 2006. HAMBURG, Germany, 3–8 September, 2006.

  2. T. B. Bliznova, Yu. G. Obolenskii, and V. A. Polkovnikov, “Mathematical Models and Algorithms of Parametric Synthesis of Actuators of Control Servoactuators of a Maneurvering Aircraft”, Izv. Ross. Akad. Nauk, Teor. Sist. Upr., No. 4, (2009) [Comp. Syst. Sci. 48 (4), (2009)].

  3. V. A. Polkovkinov, Electric, Hydraulic, and Pneumatic Servoactuators of Aircrafts and Their Limiting Dynamic Capabilities (Izd. MAI, Moscow, 20020 [in Russian].

  4. G. S. Bushgens, Aerodynamic, Stability & Controllability of Supersonic Aircraft (Nauka, Fizmatlit, Moscow, 1998) [in Russian].

    Google Scholar 

  5. V. A. Polkovkinov, V. I. Karev, S. L. Samsonovich, et al., Research Report “Study of Rational Types of Actuator of Control Servoactuators of Complex Control Systems for New Generation Aircrafts”, contract No. 29556 (MAI, Moscow, 2005).

    Google Scholar 

  6. http://www.motiontech.com.au/assets/pdf/RBE(H)%20Framless%20Motor%20(1019).pdf.

  7. A. N. Gerashchenko and S. L. Samsonovich, Pneumatic, Hydraulic, and Electric Servoactuators of Aircrafts Based on Harmonic Actuators (Mashinostroenie, Moscow, 2006) [in Russian].

    Google Scholar 

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Authors and Affiliations

  1. Moscow Aviation Institute (Technical University), Volokolamskoe sh. 4, GSP-3, A-80, Moscow, 125993, Russia

    T. B. Bliznova, V. I. Karev, Yu. G. Obolenskii, V. A. Polkovnikov & S. L. Samsonovich

  2. PC Russian Aircraft Corporation “MIG”, Pervyi Botkinskiy pr. 7, Moscow, 125284, Russia

    T. B. Bliznova, V. I. Karev, Yu. G. Obolenskii, V. A. Polkovnikov & S. L. Samsonovich

Authors
  1. T. B. Bliznova
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  2. V. I. Karev
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  3. Yu. G. Obolenskii
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  4. V. A. Polkovnikov
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  5. S. L. Samsonovich
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Additional information

Original Russian Text © T.B. Bliznova, V.I. Karev, Yu.G. Obolenskii, V.A. Polkovnikov, S.L. Samsonovich, 2009, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2009, No. 5, pp. 118–130.

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Bliznova, T.B., Karev, V.I., Obolenskii, Y.G. et al. Method and calculation of basic parameters of different types of control servoactuators using minimal installed power criterion. J. Comput. Syst. Sci. Int. 48, 788–800 (2009). https://doi.org/10.1134/S106423070905013X

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  • DOI: https://doi.org/10.1134/S106423070905013X

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