Fully magnetic attitude control subsystem for picosat platforms

被引：13

作者：

Colagrossi, Andrea ^{[1
]}

Lavagna, Michele ^{[1
]}

机构：

[1] Politecn Milan, Aerosp Sci & Technol Dept, Via La Masa 34, I-20156 Milan, Italy

来源：

ADVANCES IN SPACE RESEARCH | 2018年 / 62卷 / 12期

关键词：

Active attitude control; Magnetorquer; Picosat; Integral actuation; Global optimization methods; SATELLITES;

D O I：

10.1016/j.asr.2017.10.022

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

In this paper, the design of a fully magnetic attitude control subsystem for a picosat platform is discussed. The developed control law is based on a simple and reliable architecture, which can be easily implemented on small spacecrafts for de-tumbling and three-axis stabilization purposes. The subsystem design follows a practical engineering approach, exploiting global optimization methods, which lead to an integral actuation compliant with typical pointing accuracy requirements for picosat missions. Performance of the proposed attitude control subsystem is demonstrated by numerical simulations. (C) 2017 COSPAR. Published by Elsevier Ltd. All rights reserved.

引用

页码：3383 / 3397

页数：15

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