SATELLITE FOR RENDEZVOUS USING ELECTRIC PROPULSION THRUSTERS
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United States of America
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Issued Date -
Jan 9, 2025
app pub date -
Sep 20, 2024
filing date -
Sep 20, 2024
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Abstract
Satellite systems and methods to perform rendezvous between a servicer satellite and an on-orbit satellite, and specifically to satellite systems and methods to perform rendezvous between a servicer satellite and an on-orbit client satellite using electric propulsion thrusters. In one aspect, a servicer satellite fires thrusters to reduce a separation distance between the servicer satellite and the client satellite and to remove an angular momentum or a rotational velocity of the servicer satellite, and fires thrusters to reduce a rate of closure between the servicer satellite and the client satellite and to remove the angular momentum or the rotational velocity of the servicer satellite.
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