ATTITUDE DETERMINATION OF A SPACECRAFT USING A VERTICAL SENSOR

被引：1
|
作者：
Tkachenko, A. I. [1 ,2 ]
机构：
[1] Natl Acad Sci Ukraine, Int Res & Training Ctr Informat Technol & Syst, Kiev, Ukraine
[2] Minist Educ & Sci Ukraine, Kiev, Ukraine
来源：
SPACE SCIENCE AND TECHNOLOGY-KOSMICNA NAUKA I TEHNOLOGIA | 2016年 / 22卷 / 02期
关键词：
spacecraft; vertical sensor; orbital gyrocompass; attitude determination; angular stabilization;
D O I：
10.15407/knit2016.02.022
中图分类号：
P1 [天文学];
学科分类号：
0704 ;
摘要：
We show a possibility of a spacecraft attitude determination using the only source of information - a local vertical reference frame - in a condition of the vehicle's angular stabilization by means of considerable control torques.
引用
收藏
页码：22 / 28
页数：7
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