In-flight alignment of a strapdown inertial navigation system of an unmanned aerial vehicle

被引：0
|
作者：
K. K. Veremeenko
V. M. Savel’ev
机构：
[1] State Research Institute of Aviation Systems,
[2] Moscow Institute of Aviation,undefined
来源：
Journal of Computer and Systems Sciences International | 2013年 / 52卷
关键词：
Navigation System; Unmanned Aerial Vehicle; Attitude Angle; System Science International; Inertial Measurement Unit;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The alignment system of a strapdown inertial navigation system for an unmanned aerial vehicle installed on a carrier aircraft is studied. The aim is to develop alignment techniques for the strapdown inertial navigation system that improve the accuracy of alignment and reduce the alignment time. A technique for constructing the initial alignment system for a strapdown inertial navigation system of an unmanned aerial vehicle is proposed.
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页码：106 / 116
页数：10
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