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

被引：0
作者：
Anshakov G.P. [1 ]
Belousov A.I. [1 ]
Sedel’nikov A.V. [1 ]
Gorozhankina A.S. [1 ]
机构：
[1] Samara University, Moskovskoe sh. 34, Samara
来源：
Russian Aeronautics | 2018年 / 61卷 / 3期
关键词：
control system; electrothermal thruster; microacceleration level; spacecraft;
D O I：
10.3103/S1068799818030054
中图分类号：
学科分类号：
摘要：
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. © 2018, Allerton Press, Inc.
引用
收藏
页码：347 / 354
页数：7
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