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...
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Main Authors | , , , , |
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Format | Patent |
Language | Chinese English |
Published |
02.02.2024
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Subjects | |
Online Access | Get full text |
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