GAIN SELECTION FOR ATTITUDE STABILIZATION OF EARTH-POINTING SPACECRAFT USING MAGNETORQUERS

被引：0

作者：

Celani, Fabio ^{[1
]}

机构：

[1] Sapienza Univ Rome, Sch Aerosp Engn, Via Salaria 851, I-00138 Rome, Italy

来源：

FOURTH IAA CONFERENCE ON UNIVERSITY SATELLITE MISSIONS AND CUBESAT WORKSHOP 2017 | 2018年 / 163卷

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

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 gain matrices are determined through the numerical solution of a periodic linear quadric regulator problem. A case study shows the effectiveness of the considered controller gain selection.

引用

页码：307 / 318

页数：12

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