Attitude control system for the first Swedish nanosatellite "MUNIN"

被引：19
|
作者：
Ovchinnikov, M [1 ]
Pen'kov, V [1 ]
Norberg, O [1 ]
Barabash, S [1 ]
机构：
[1] MV Keldysh Appl Math Inst, Moscow 125047, Russia
来源：
ACTA ASTRONAUTICA | 2000年 / 46卷 / 2-6期
关键词：
The applied aspects of work are being supported by the Swedish Institute of Space Physics; Kiruna Division; Sweden. Also this work is supported by RBSF (projects 97-01-00910 and 96-15-97229). Students of the Moscow Institute for Physics & Technology took part in this project;
D O I：
10.1016/S0094-5765(99)00226-X
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The paper describes the passive magnetic attitude control system developed for the Swedish nanosatellite MUNIN, its composition, and the results of the mathematical modeling of the satellite motion around its center of mass under the effects of external torques and control by this attitude control system. The satellite MUNIN is to be oriented along the local vector of intensity of the geomagnetic field. The problems, which are expediently considered hereafter are formulated too. (C) 2000 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码：319 / 326
页数：8
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