IGSO satellite Kepler orbital element correction method based on perigee angular distance correction

The invention provides an IGSO satellite Kepler orbital element correction method based on perigee angular distance correction, and belongs to the field of satellite navigation system constellation simulation. According to the method, six ephemeris of Kepler orbits of a satellite are used as simulat...

Full description

Saved in:
Bibliographic Details
Main Authors CUI MIAO, YU BAOGUO, YI QINGWU, KONG XIANGYU, WU CAILUN
Format Patent
LanguageChinese
English
Published 02.02.2024
Subjects
Online AccessGet full text

Cover

Loading…