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

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

doi:10.3103/S1068799818030054

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

Authors: Anshakov G.P.¹, Belousov A.I.¹, Sedel’nikov A.V.¹, Gorozhankina A.S.¹
Affiliations:
1. Samara University
Issue: Vol 61, No 3 (2018)
Pages: 347-354
Section: Flight Dynamics and Control of Flight Vehicles
URL: https://journal-vniispk.ru/1068-7998/article/view/230581
DOI: https://doi.org/10.3103/S1068799818030054
ID: 230581

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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.