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

页码：15 / 24

页数：9

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