METHOD FOR PLANNING A SATELLITE MANEUVER
The invention relates to a method for planning a satellite maneuver, in particular for planning an orbital change of a satellite orbit after the completion of a mission (240), with the satellite (220) having a drive unit (150) with a ground-based power supply, at least comprising the steps of: - con...
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Main Authors | , , , |
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Format | Patent |
Language | English French German |
Published |
06.09.2023
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Subjects | |
Online Access | Get full text |
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Summary: | The invention relates to a method for planning a satellite maneuver, in particular for planning an orbital change of a satellite orbit after the completion of a mission (240), with the satellite (220) having a drive unit (150) with a ground-based power supply, at least comprising the steps of: - configuring at least one ground-based laser system (100) for producing a laser beam, in particular laser pulses; - configuring at least one laser ground station (200) including the at least one laser system (100); - designing an optical transmission path (120) for transmitting the laser pulses from the at least one ground station (200) to the satellite (220); - configuring the satellite-based drive unit (150), in particular an ablation drive where mass is removed from the drive unit (150) by means of the laser pulses; - determining a trajectory attainable by means of the drive unit (150), with the steps being run through in an iteration until the desired orbital change has been achieved. |
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Bibliography: | Application Number: EP20210798593 |