CubeSat Constellation Design for Intersatellite Linking
This thesis investigates the concept of controlling a CubeSat constellation in low-Earth orbit. Low-Earth orbits are considered because the torque used for satellite control is supplied with magnetorquers, and the closer the satellite is to Earth’s magnetic field the more control gain can be supplie...
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| Format: | Others |
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Scholar Commons
2019
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| Online Access: | https://scholarcommons.usf.edu/etd/7987 https://scholarcommons.usf.edu/cgi/viewcontent.cgi?article=9184&context=etd |