The method involves determining a deviation between a current state vector of a satellite and a predetermined path (104), and determining Lagrange multipliers (105) from the current state vector of the satellite, the determined deviation and parameters of a predefined control law. Parameters of a current control law of an electrical motor are determined (106) by the multipliers and by derivation of a parameter representative of a motor effect on a real path. The motor parameters are controlled (107) from the current control law. An independent claim is also included for a satellite.
Procédé et système de mise à poste d'un satellite
Method and system for inserting a satellite into orbit
Verfahren und System zum Einbringen eines Satelliten in einen Orbit
2018-11-07
Patent
Electronic Resource
French
IPC: | B64G Raumfahrt , COSMONAUTICS |
European Patent Office | 2017
|European Patent Office | 2017
|European Patent Office | 2016
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