
Improving sgp4 orbit propagation
Author(s) -
Bogdan Perviy
Publication year - 2019
Publication title -
sistemnì tehnologìï
Language(s) - English
Resource type - Journals
eISSN - 2707-7977
pISSN - 1562-9945
DOI - 10.34185/1562-9945-6-125-2019-07
Subject(s) - orbit (dynamics) , computer science , low earth orbit , span (engineering) , algorithm , aerospace engineering , engineering , satellite , structural engineering
The review reflects a comparison between several studies on improving the orbit propagataion accuracy using space objects’ TLE-elements. The study is done to identify a technique that can be applied to enhance the SGP4 model despite increasing the propagation span. The method used in this study is by comparing the techniques that have been used by other researchers for the orbit propagation model. From the review that has been done, a beta regression technique is found to be a suitable technique.