| 摘要 |
The invention relates to a method for controlling a set of at least two satellites adapted to provide a service used by at least one portion of the set of the said satellites at a given moment, in which, continuously or pseudo-continuously, a mean value (.OMEGA.m(t)) of the longitudes (.OMEGA.i(t)) of the respective ascending nodes of each satellite is computed, and, for each satellite, a correction of trajectory of the satellite is applied by regulating the longitude of the ascending node (.OMEGA.i(t)) on a setpoint equal to the said current mean value (.OMEGA.m(t)). |
