Perspectives of Integrated Inertial-Satellite Systems Development of Civil Aviation Aircraft

被引：0
|
作者：
Sineglazov, V. M. [1 ]
Zaharin, F. M. [1 ]
机构：
[1] Natl Aviat Univ, Kiev, Ukraine
来源：
2012 2ND INTERNATIONAL CONFERENCE METHODS AND SYSTEMS OF NAVIGATION AND MOTION CONTROL (MSNMC) | 2012年
关键词：
inertial navigation systems; Global Positioning System; aircraft; integration;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Using an inertial navigation system and Global Positioning System together is preferable to using any of them separately. Derived benefits depend on the level of combining information. Inertial navigation systems/Global Positioning System integration architectures are defined as separate, loosely and tightly coupled, deeply integrated configurations.
引用
收藏
页码：9 / 12
页数：4
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