A method of deploying a constellation of satellites includes using a single launch vehicle to deploy a plurality of satellites at an initial altitude on a same initial orbit, controlling said satellites such that an altitude of some of the satellites is modified while their inclination relative to an equatorial plane and a type of trajectory, of the some of the satellites, remains identical so that each satellite reaches a drift altitude selected from a drift set, with orbits of various satellites shifting relative to one another, and controlling the satellites to be moved sequentially in order to reach a same final altitude, said sequential movement being performed in such a manner that the satellites describe final orbits having trajectories with a same angle of inclination relative to the equatorial plane, a same apogee and perigee, and the same final altitude but presenting distinct longitudes for ascending nodes.
METHOD FOR DEPLOYING A SATELLITE CONSTELLATION
2017-02-16
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Europäisches Patentamt | 2020
|Europäisches Patentamt | 2020
|Europäisches Patentamt | 2020
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