Gain Selection for Attitude Stabilization of Earth-Pointing Spacecraft Using Magnetorquers

被引：0
|
作者：
Fabio Celani
机构：
[1] Sapienza University of Rome,School of Aerospace Engineering
来源：
Aerotecnica Missili & Spazio | 2021年 / 100卷 / 1期
关键词：
Spacecraft attitude stabilization; Magnetorquers; PD-like control; Matrix gains;
D O I：
10.1007/s42496-020-00062-2
中图分类号：
学科分类号：
摘要：
This paper considers a feedback control law that achieves attitude stabilization for Earth-pointing spacecraft using only magnetorquers as torque actuators. The control law is proportional derivative (PD)-like with matrix gains, and it guarantees asymptotic stability. The PD matrix gains are determined through the numerical solution of a periodic linear quadric regulator problem. A case study shows the effectiveness of the considered control law, and specifically of the gain selection method, in a simplified simulation scenario.
引用
收藏
页码：15 / 24
页数：9
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