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Russian Aeronautics

, Volume 61, Issue 3, pp 347–354 | Cite as

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

  • G. P. Anshakov
  • A. I. BelousovEmail author
  • A. V. Sedel’nikov
  • A. S. Gorozhankina
Flight Dynamics and Control of Flight Vehicles
  • 6 Downloads

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.

Keywords

spacecraft microacceleration level control system electrothermal thruster 

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Copyright information

© Allerton Press, Inc. 2018

Authors and Affiliations

  • G. P. Anshakov
    • 1
  • A. I. Belousov
    • 1
    Email author
  • A. V. Sedel’nikov
    • 1
  • A. S. Gorozhankina
    • 1
  1. 1.Samara UniversitySamaraRussia

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