A system for receiving satellite signals disrupted by at least one interference source and by a thermal noise, comprising: - means for receiving said satellite signals; - means for filtering said satellite signals so as to suppress the disruption of said interference sources; - first means for determining a first inter-correlation matrix of said satellite signals; - adding means for respectively adding a first coefficient to at least one element of the diagonal of said first inter-correlation matrix so as to obtain a second inter-correlation matrix; - second means for determining, on the basis of said second inter-correlation matrix, second coefficients used by said filtering means, said second determination means using a space-time process, characterised in that it also comprises: - means for detecting a first power of said thermal noise and a second power of all of the interference sources on the basis of an automatic gain control device or of said first inter-correlation matrix; - third means for dynamically determining the value of said first coefficients, on the basis of the first power, of said second power, of a desired rejection level and of a power threshold for the interference sources, said third means comprise computation means adapted to compute said first coefficients using the following relation: C i j = P noise i + Δ clamping R max i, where C(i, j) represents the first coefficient to be added to the element of the diagonal that corresponds to the receiver i and to the sample j of said first matrix, P noise (i) represents the thermal noise of the receiver i, R max represents the determined level of maximum rejection, for which the rejection must be carried out by the system, and Δ clamping (R max, i) is obtained by the following relations: Δ clamping R max i = 0 if P int i − P noise i < R max Δ clamping R max i = R max − P int i − P noise i if P int i − P noise i ≥ R max, where P int (i) represents the power of the interferences received by the receiver i. - means for receiving said satellite signals; - means for filtering said satellite signals so as to suppress the disruption of said interference sources; - first means for determining a first inter-correlation matrix of said satellite signals; - adding means for respectively adding a first coefficient to at least one element of the diagonal of said first inter-correlation matrix so as to obtain a second inter-correlation matrix; - second means for determining, on the basis of said second inter-correlation matrix, second coefficients used by said filtering means, said second determination means using a space-time process, - means for detecting a first power of said thermal noise and a second power of all of the interference sources on the basis of an automatic gain control device or of said first inter-correlation matrix; - third means for dynamically determining the value of said first coefficients, on the basis of the first power, of said second power, of a desired rejection level and of a power threshold for the interference sources, said third means comprise computation means adapted to compute said first coefficients using the following relation: C i j = P noise i + Δ clamping R max i, where C(i, j) represents the first coefficient to be added to the element of the diagonal that corresponds to the receiver i and to the sample j of said first matrix, P noise (i) represents the thermal noise of the receiver i, R max represents the determined level of maximum rejection, for which the rejection must be carried out by the system, and Δ clamping (R max, i) is obtained by the following relations: Δ clamping R max i = 0 if P int i − P noise i < R max Δ clamping R max i = R max − P int i − P noise i if P int i − P noise i ≥ R max, where P int (i) represents the power of the interferences received by the receiver i.