Altimeter + INS/Giant LEO Constellation Dual-Satellite Integrated Navigation and Positioning Algorithm Based on Similar Ellipsoid Model and UKF

Altimeter + INS/Giant LEO Constellation Dual-Satellite Integrated Navigation and Positioning Algorithm Based on Similar Ellipsoid Model and UKF

To solve the problem of location service interruption that is easily caused by incomplete visual satellite environments such as occlusion, urban blocks and mountains, we propose an altimeter + inertial navigation system (INS) + giant low earth orbit (LEO) dual-satellite (LEO2) switching integrated n...

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Bibliographic Details
Main Authors: Lvyang Ye, Yikang Yang, Xiaolun Jing, Hengnian Li, Haifeng Yang, Yunxia Xia
Format: Article
Language:English
Published: MDPI AG 2021-10-01
Series:Remote Sensing
Subjects:
LEO
altimeter
double star
similar ellipsoid
integrated navigation
switching
Online Access:https://www.mdpi.com/2072-4292/13/20/4099

Internet

https://www.mdpi.com/2072-4292/13/20/4099

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