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...

詳細記述

書誌詳細
出版年:Remote Sensing
主要な著者: Lvyang Ye, Yikang Yang, Xiaolun Jing, Hengnian Li, Haifeng Yang, Yunxia Xia
フォーマット: 論文
言語:英語
出版事項: MDPI AG 2021-10-01
主題:
オンライン・アクセス:https://www.mdpi.com/2072-4292/13/20/4099