Nanosatellite reflector for optical calibrations: Attitude control and determination aspects

被引：3
|
作者：
Shargorodsky, V
Shevchenko, V
Ovchinnikov, M
Penkov, V
Mirer, S
Nemuchinsky, R
机构：
[1] SRIPDE SDEC, Moscow 111250, Russia
[2] RAS, KIAM, Moscow 125047, Russia
[3] Moscow Phys Tech Inst, Dolgoprudnyi 141700, Moscow Region, Russia
来源：
NEW TRENDS IN SPACE GEODESY | 2002年 / 30卷 / 02期
基金：
俄罗斯基础研究基金会;
关键词：
D O I：
10.1016/S0273-1177(02)00304-6
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Nanosatellite REFLECTOR has been designed to provide an orbital reference target for collaborative optical sensing, imaging, and tracking experiments with space objects. The satellite hosts well-calibrated laser reflectors that provide a unique target for experiments involving laser illumination. A passive gravity-gradient attitude control system is used to ensure a given angular motion of the satellite. A problem of attitude control system development and ideas of attitude determination without on-board sensors are discussed. (C) 2002 COSPAR. Published by Elsevier Science Ltd. All rights reserved.
引用
收藏
页码：337 / 343
页数：7
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