Orbit Determination via a Deeply- Coupled UKF/GNSS Filter

This paper is dedicated to determining the orbit of a satellite by using Unscented Kalman Filter (UKF), in which, a GNSS is used as the observation sensor. During this goal, firstly we have simulated the satellite orbit; considering oblations effect. Secondly, exploiting a nonlinear model of orbit d...

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Bibliographic Details

Published in:	فصلنامه علوم و فناوری فضایی
Main Authors:	MohammadAli Amiri Atashgah, Hamid Gazerpour, seyed Amirreza Roghangir
Format:	Article
Language:	Persian
Published:	Aerospace Research Institute 2016-11-01
Subjects:	orbit estimation gps/gnss unscented kalman filter (ukf) gnss error prediction
Online Access:	https://jsst.ias.ir/article_44472_82d57b3de3b310bdfd7b33d32dc189bf.pdf