卫星姿态控制推力器布局分析

doi:10.3969/j.issn.1674-1579.2013.06.005

Abstract

Abstract: Aimed at the problem of choosing appropriate amount and suitable arrangement of thrusters for satellite attitude control, four different configurations of thrusters are summarized. Thruster burn time is given under phase-plane control, and the design criterion is proposed with comparing of control accuracy, fuel consumption and reliability under different configurations. This criterion shows that the reliability and fuel consumption are the primary reference in the design of thruster configuration.

Key words: configuration, burn time, fuel consumption, reliability

CLC Number:

V448.2

GU Peng, WANG Da-Yi, LIU Cheng-Rui. Analysis on Thrusters Configuration of Satellite Attitude Control[J]., 2013, 39(6): 23-28.

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2013.06.005

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2013/V39/I6/23

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Analysis on Thrusters Configuration of Satellite Attitude Control

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