Analysis Method for the Mass Center of Low Earth Orbit Remote Sensing in Orbit

A real-time method for estimating the mass center of low earth orbit (LEO) remote sensing satellite in orbit is introduced in this paper. LEO remote sensing satellite requires highly on calculating the position of its mass center, due to the need of precise orbit determination and attitude control....

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Bibliographic Details
Published inJournal of physics. Conference series Vol. 1877; no. 1; p. 12027
Main Authors Jinghao, Xu, Wenjing, Ding, Lei, Zhang, Zhilong, Zhang
Format Journal Article
LanguageEnglish
Published Bristol IOP Publishing 01.04.2021
Subjects
Antenna arrays
Attitude control
Centroids
Data transmission
Low earth orbits
Mathematical analysis
Orbit determination
Physics
Position sensing
Remote sensing
Solar arrays
Solar collectors
Spacecraft
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Summary:A real-time method for estimating the mass center of low earth orbit (LEO) remote sensing satellite in orbit is introduced in this paper. LEO remote sensing satellite requires highly on calculating the position of its mass center, due to the need of precise orbit determination and attitude control. This article offers an analysis method for the factors that play a leading role in the change of the centroid of satellite in orbit, which are the consuming of satellite fuel, the circulation of satellite-to-ground data transmission antenna and rotation of solar arrays. The parameters for calculating the centroid of LEO remote sensing satellite are defined, and a formula for computing the position of the satellite mass center in orbit is proposed.
Bibliography:ObjectType-Conference Proceeding-1
SourceType-Scholarly Journals-1
content type line 14
ISSN:1742-6588
1742-6596
DOI:10.1088/1742-6596/1877/1/012027