Integrated inertial-satellite navigation system corrected with observations of a single star

被引：0
|
作者：
A. S. Devyatisil’nyi
K. A. Chislov
机构：
[1] Russian Academy of Sciences (IAPU DVO RAN),Institute of Automation and Control Processes, Far Eastern Branch
来源：
Measurement Techniques | 2013年 / 56卷
关键词：
inertial navigation; satellite navigation and astrosystems; inverse problem;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Models for integration of inertial, satellite, and astro- information are proposed and studied in the framework of the correction problem for inertial navigation systems. Results are presented from numerical simulations characterizing the numerical stability and efficiency with which the problem can be solved under conditions of finite measurement accuracy.
引用
收藏
页码：355 / 358
页数：3
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