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Efficiency Estimation of Electrothermal Thrusters Use in the Control System of the Technological Spacecraft Motion

  • Flight Dynamics and Control of Flight Vehicles
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Abstract

The influence of various control systems of the orbital motion of a technological spacecraft on the level of microacceleration of its internal environment is simulated. Conclusions are drawn about the effectiveness of control systems with different actuators for realization of certain gravitationally sensitive processes onboard a spacecraft.

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Authors and Affiliations

  1. Samara University, Moskovskoe sh. 34, Samara, 443086, Russia

    G. P. Anshakov, A. I. Belousov, A. V. Sedel’nikov & A. S. Gorozhankina

Authors
  1. G. P. Anshakov
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  2. A. I. Belousov
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  3. A. V. Sedel’nikov
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  4. A. S. Gorozhankina
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Corresponding author

Correspondence to A. I. Belousov.

Additional information

Original Russian Text © G.P. Anshakov, A.I. Belousov, A.V. Sedel’nikov, A.S. Gorozhankina, 2018, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2018, No. 3, pp. 28–34.

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Anshakov, G.P., Belousov, A.I., Sedel’nikov, A.V. et al. Efficiency Estimation of Electrothermal Thrusters Use in the Control System of the Technological Spacecraft Motion. Russ. Aeronaut. 61, 347–354 (2018). https://doi.org/10.3103/S1068799818030054

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  • DOI: https://doi.org/10.3103/S1068799818030054

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