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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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Autors principals: Zhenglong Lu, Jie Li, Xi Zhang, Kaiqiang Feng, Xiaokai Wei, Debiao Zhang, Jing Mi, Yang Liu
Format: Artigo
Idioma:Inglês
Publicat: MDPI AG 2020-01-01
Col·lecció:Sensors
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Accés en línia:https://www.mdpi.com/1424-8220/20/2/512
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