A New In-Flight Alignment Method with an Application to the Low-Cost SINS/GPS Integrated Navigation System

The optimization-based alignment (OBA) methods, which are implemented by the optimal attitude estimation using vector observations—also called double-vectors—have proven to be effective at solving the in-flight alignment (IFA) problem. However, the traditional OBA methods are not...

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Main Authors: Zhenglong Lu, Jie Li, Xi Zhang, Kaiqiang Feng, Xiaokai Wei, Debiao Zhang, Jing Mi, Yang Liu
Format: Artigo
Jezik:Inglês
Izdano: MDPI AG 2020-01-01
Serija:Sensors
Teme:
in-flight alignment
integrated navigation system
optimization-based alignment
Online dostop:https://www.mdpi.com/1424-8220/20/2/512
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