Coverage Analysis in Case of Faults of Some Satellites in Low Earth Orbit Satellite Constellations

In this paper we analyze the coverage performance of satellite constellation specially in low earth orbit. First of all we analyze the various possible configuration of combinations of failures of satellites in the same orbital plane or in different orbital planes when one satellite or a number of satellites are in faults. To evaluate the performances of constellation we use one parameter, which is the maximum non-visibility time at one receiver position on earth by using simulation software. Also we have simulated by varying the latitude of the receiver position from 0 degree to 90 degrees to analyze the coverage performance variations depending on the receiver position on earth. According to the results of the simulations we compare the maximum non-visibility time depending on the configuration of failure of satellites and identified the worst case of combination of satellite failures in satellite constellation. Finally we evaluate the some orbital maneuver strategy, (phase changing in the same orbital plane), to minimize the non-visibility time on earth in case of failure of number of satellites.

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Publication Details

Journal
Digital Commons - USU (Utah State University)
Published
2025-08-18
DOI
https://doi.org/10.26077/m38y-n025
Citations
3
Primary Topic
Spacecraft Design and Technology
Type
article
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article

Coverage Analysis in Case of Faults of Some Satellites in Low Earth Orbit Satellite Constellations

Chan-Wang Park
3 citations
Digital Commons - USU (Utah State University)
Spacecraft Design and Technology
article

Coverage Analysis in Case of Faults of Some Satellites in Low Earth Orbit Satellite Constellations

Chan-Wang Park
article en
3 citations

Abstract

In this paper we analyze the coverage performance of satellite constellation specially in low earth orbit. First of all we analyze the various possible configuration of combinations of failures of satellites in the same orbital plane or in different orbital planes when one satellite or a number of satellites are in faults. To evaluate the performances of constellation we use one parameter, which is the maximum non-visibility time at one receiver position on earth by using simulation software. Also we have simulated by varying the latitude of the receiver position from 0 degree to 90 degrees to analyze the coverage performance variations depending on the receiver position on earth. According to the results of the simulations we compare the maximum non-visibility time depending on the configuration of failure of satellites and identified the worst case of combination of satellite failures in satellite constellation. Finally we evaluate the some orbital maneuver strategy, (phase changing in the same orbital plane), to minimize the non-visibility time on earth in case of failure of number of satellites.

Digital Commons - USU (Utah State University)
Université de Lille (FR)
Climate action
Spacecraft Design and Technology
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Coverage Analysis in Case of Faults of Some Satellites in Low Earth Orbit Satellite Constellations — Chan-Wang Park · Digital Commons - USU (Utah State University) (2025) | TGRS Research Map | TGRS