Tightly Coupled Integrated Navigation Algorithm for Hypersonic Boost-Glide Vehicles in the LCEF Frame

According to the trajectory characteristics of hypersonic boost-glide vehicles, a tightly coupled integrated navigation algorithm for hypersonic vehicles based on the launch-centered Earth-fixed (LCEF) frame is proposed. First, the strapdown inertial navigation mechanization algorithm and discrete u...

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Bibliographic Details

Published in:	Aerospace
Main Authors:	Kai Chen, Sensen Pei, Fuqiang Shen, Shangbo Liu
Format:	Article
Language:	English
Published:	MDPI AG 2021-04-01
Subjects:	hypersonic vehicle boost-glide trajectory launch-centered Earth-fixed frame strapdown inertial navigation tightly coupled integrated navigation
Online Access:	https://www.mdpi.com/2226-4310/8/5/124